N938DL

Part: BATTERY — INOPERATIVE (SMOKE DETECTOR) · airframe 73,874 hrs · 54,764 cycles

LAVATORY SMOKE DETECTOR WILL NOT TURN OFF. REPLACED THE SMOKE DETECTOR BATTERY AND TESTED GOOD IAW AMM 26-21.

Part: CONNECTOR — DISCONNECTED (EMERGENCY LIGHTS) · airframe 73,855 hrs · 54,754 cycles

EMERGENCY LIGHT AT 23 DE INOPERATIVE. FOUND THE CONNECTOR DISCONNECTED. RECONNECTED.

Part: BATTERY — DISCHARGED (CABIN) · airframe 73,848 hrs · 54,750 cycles

OVERHEAD EMERGENCY LIGHTS BETWEEN ROWS 11 AND 15 INOP. REPLACED BATTERIES AT BATTERY PACK ROW 12 RIGHT. OPS CKS GOOD PER AMM 33-50.

Part: DOOR — EXCESS PLAY (NLG) · airframe 73,477 hrs · 54,456 cycles

CREW REPORTED DURING TAKE OFF, THE CREW REPORTED A NOSE WHEEL VIBRATION AND RUBBER ODOR AT V1. FLT CONTINUED. AFTER LANDING, THE TIRE TREAD WAS INTACT WITH NO VISIBLE DAMAGE. FOUND THE LT NOSE GEAR DOOR WITH EXCESSIVE PLAY. ADJUSTED DOOR AND LUBRICATED DOORS & GEAR. REPLACED BOTH NOSE TIRES.

Part: FUSE — INOPERATIVE (EMERGENCY LIGHTS) · airframe 72,957 hrs · 54,033 cycles

EMERGENCY LIGHTS IN AFT SECTION OF CABIN ARE INOPERATIVE. REPLACED THE FUSES IN THE AFT BATTERY PACK. CHECKED GOOD IAW AMM 33-53.

Part: LAMP — INOPERATIVE (EMERGENCY LIGHT) · airframe 72,827 hrs · 53,924 cycles

RT EXTERIOR EMERGENCY LIGHT INOPERATIVE. REPLACED THE LAMPS, CHECKED GOOD.

Part: CONNECTOR — FAILED (EMERGENCY LIGHTS) · airframe 67,155 hrs · 49,896 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE EMERGENCY LIGHTS AT ROW 4C, 24E, 28E, AND 33E IN THE CABIN WERE INOPERATIVE. MAINTENANCE FOUND A FAILED CONNECTOR IN THE WIRE HARNESS AND REPLACED IT. THE FUNCTIONAL CHECK OF THE SYSTEM WAS GOOD. LP 1892209

Part: LIGHT — INOPERATIVE (CABIN) · airframe 64,690 hrs · 48,118 cycles

DURING LINE CHECK, MAINTENANCE FOUND THAT THE RED EMERGENCY LIGHT FOR EXIT ROW 24DE WAS INOPERATIVE. MAINTENANCE REPLACED THE LIGHT ASSEMBLY AND PERFORMED A SATISFACTORY FUNCTIONAL CHECK OF IT.

Part: SKIN — CRACKED (BS 1380) · airframe 64,486 hrs · 48,001 cycles

ACFT SKIN HAS A .3750" CRACK AT FASTENER HOLE, BS 1380, 1 INCH ABOVE LONGERON 13 LT. CONFIRMED WITH HFEC, SUMMARY OF EMPOWER NRC 68; REPAIRED IAW PRI ER/A 524139-14, REV 0-REV 1 BY DAMAGE CUTOUT AND DOUBLER INSTALLATION. DOUBLER WAS MADE LARGER FOR AREA TO INCORPORATE PREVIOUS EXISTING REPAIR. REPAIR IS IDENTIFIED AS TIME LIMITED IAW PRI STEP 10 OF PRI ER/A 524139-14, REV 0 AND REV 1. FINAL ER/A PENDING.

Part: SKIN — CRACKED (BS 1437) · airframe 64,486 hrs · 48,001 cycles

FUSELAGE EXTERIOR, CRACK EMINATING FROM FASTENER AT BS 1437 JUST BELOW RT SKATE ANGLE. HFEC VERIFIED, REF NR 102, COMPLETED REPAIR IAW PRI 524140-14, REV ORIG WAITING FOR FINAL ER/A.

Part: LANYARD — MISINSTALLED (ESCAPE SLIDE) · airframe 61,053 hrs · 45,614 cycles

INSPECTION DISCOVERED THAT THE EMERGENCY ESCAPE SLIDE IN THE TAILCONE HAD AN IMPROPERLY INSTALLED LANYARD. THE TAILCONE SLIDE AND LANYARD WERE INSTALLED CORRECTLY.

Part: RELEASE CABLE — FRAYED (TAIL CONE) · airframe 61,053 hrs · 45,614 cycles

MX DISCOVERED THAT THE TAILCONE RELEASE CABLE WAS FRAYED BEYOND ALLOWABLE LIMITS. THE CABLE WAS REPLACED AND THE SYSTEM WAS RIGGED TO SPECIFICATIONS.

Part: BEAM — CORRODED (BS 1221) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON BEAM BS 1221 BETWEEN LONGERONS 30 AND 28 RIGHT AT AFT CARGO COMPARTMENT (C3). FASTENERS AND CORROSION WERE REMOVED AND REWORKED AREA WAS TREATED AND PAINTED. FASTENERS WERE INSTALLED IAW SRM 51-30-05 AND 51-10-03 PARA 14, 21 AND 26.

Part: TEE FITTING — CRACKED (MLG DOOR FRAME) · airframe 61,052 hrs · 45,613 cycles

DETAILED INSPECTION PERFORMED. CRACKED TEE OF LT MLG JAMB WAS FOUND. REMOVED AND NEW TEE WAS DRILLED, TREATED, PAINTED AND INSTALLED IAW SRM 51-30-02, 51-10-4, 51-10-3 AND DWG 5936395, REV BF.

Part: DOOR FRAME — CORRODED (BS 652-677) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LOWER DOOR FRAME BEAM AT MID CARGO COMPARTMENT BETWEEN BS 652 TO 677. REPAIRED IAW ER/A 506669-14 REV O.

Part: WINDOW FRAME — DAMAGED (BS 465-484) · airframe 61,052 hrs · 45,613 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME BTW BS 465-484 FWD EDGE AND AFT UPPER CORNER. AREA WAS BLEND OUT MEASURE TREATED IAW ER/A 506655-14, REV ORIG.

Part: WINDOW FRAME — DAMAGED (BS 370-389) · airframe 61,052 hrs · 45,613 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME BETWEEN BS 370-389 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14, REV ORIG .

Part: BEARING — WORN (TAILCONE RELEASE) · airframe 61,052 hrs · 45,613 cycles

DURING INSPECTION OF THE TAILCONE RELEASE SYSTEM, MX FOUND THE RELEASE CAM BEARING WORN BEYOND LIMITS, ALLOWING EXCESSIVE FREE PLAY. THE CAM BEARING WAS REPLACED. FOLLOW UP FUNCTIONAL CHECKED GOOD.

Part: WINDOW FRAME — NICKED (BS 1193-1212) · airframe 61,052 hrs · 45,613 cycles

NICK ON LT WINDOW BELT FRAME BTW BS 1193-1212 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14 REV ORIG.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,052 hrs · 45,613 cycles

CRACKED OUTER PAN ON AFT EDGE BELOW TO STOP FITTING NR 3 OF FWD CARGO COMPARTMENT DOOR AFT EDGE REF NRC (T0 262757) PAN WAS REPAIRED IAW SRM 52-05D FIG 50 RII COMPLETED.

Part: WINDOW FRAME — DAMAGED (BS 636-655) · airframe 61,052 hrs · 45,613 cycles

SCRATCH ON LT WINDOW BELT FRAME BETWEEN BS 636-655 AFT LOWER CORNER. AREA WAS BLEND OUT, MEASURE, AND TREATED IAW ER/A 506655-14, REV ORIG.

Part: DUCT — CRACKED (E/E COOLING) · airframe 61,052 hrs · 45,613 cycles

CRACKED RADIO RACK COOLING EXHAUST DUCT ON FWD CORNERS. REPAIRED IAW ERA 464964-14 MA REV ORIG.

Part: LONGERON — CORRODED (BS 1290 L24L) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LONGERON 24L BS 1290. REPLACED LONGERON IAW SRM 53-02, FIG 18.

Part: STRINGER — CORRODED · airframe 61,052 hrs · 45,613 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER BS 465 TO 535 BTW STA X=-50 TO -60. REPLACED IAW SRM 53-05, FIG 827D AND 53-05, FIG 131 & DWG 9930538, REV CF.

Part: SKIN — CORRODED (BS 1114-1119) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON FUSELAGE SKIN UNDER WING TO FUSELAGE FILLET FAIRING FROM BS 1114 TO 1119 L24 TO 30 LT. REPAIRED IAW SRM 53-04 P57.

Part: CUSP WEB — CORRODED (BS 787-804) · airframe 61,052 hrs · 45,613 cycles

CORROSION OUT OF LIMITS ON LT CUSP WEB FROM STA 787- 804 BETWEEN X=54 TO X=60 AT PAX CABIN WITH REF OM828H CARD 33, ZONE 58 AND NRC (T0 262756). REF NRC (T0 263839) CUSP WEB WAS REPAIRED IAW SRM 53-01, FIG 4.

Part: CUSP WEB — CORRODED (BS 579-983) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LT CUSP WEB BTW X=54-60 FROM STA Y=579-983. REPAIRED IAW SRM 53-05, FIG 131A-10.

Part: LONGERON — CRACKED (BS 1309 L8R) · airframe 61,052 hrs · 45,613 cycles

CRACK ON LONGERON 8R BS 1309 . REPAIRED IAW SRM 53-02, FIG 18 AND DWG 5936436.

Part: CUSP WEB — CORRODED (BS 938-1020) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON PREVIOUS REPAIR DOUBLER AT RT CUSP WEB BTW X=-54 TO X=-60 FROM BS 938-1020. CUSP WEB REPAIRED IAW 53-05 D FIG 827D AND ERA 398191-14MA REV B ASSOCIATED ER/A 39-819114 ADDED FOR AC 0938.

Part: CUSP WEB — CORRODED (BS 755-769) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE BETWEEN BS 769 TO 755 X= -54 AND X= -60. REPAIRED IAW DRD 53-05D, FIG 827D.

Part: INTERCOSTAL — CORRODED (BS 1309-1322) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON INTERCOSTAL FROM STA BS 1309 TO 1322. REMOVED AND INSTALLED NEW INTERCOSTALS IAW SLM 51-30-2.

Part: SKIN — CRACKED (FUSELAGE) · airframe 61,052 hrs · 45,613 cycles

CRACK ON FUSELAGE SKIN FWD STAIRWAY DOOR JAMB AFT LWR CORNER. CRACK ON FUSELAFE SKIN ON FWD STAIRWAY DOOR JAMB AFT LOWER CORNER WAS REPAIRED IAW ERA/A 506635-14AD REV ORIG.

Part: SUPPORT — CRACKED (BS 560-598) · airframe 61,052 hrs · 45,613 cycles

CRACKED LT SLANT SUPPORTS STA Y=560 AND RT STA Y=560, 598 AT MID CARGO COMPARTMENT (C2) REF NRC: (T0 263134). SLANT SUPPORT WERE REPLACED IAW ERA 413029-14MA REV:B ASSOCIATED ER/A 41-302914 ADDED FOR AC 0938.

Part: LONGERON — CRACKED (BS 1380) · airframe 61,052 hrs · 45,613 cycles

CRACKED LONGERON 13 LT BS 1380. REPLACED IAW SRM 51-30-2, 51-30-5 AND 53-02 FIG 18, DDWG 5911433 REV.

Part: CUSP WEB — CORRODED (BS 987-1054) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LT CUSP WEB UPPER LOWER SURFACE BETWEEN BS 987 TO 1054 X=54 TO X=60. REPAIRED IAW SRM 53-05.

Part: LONGERON — CORRODED (BS 1297-1323) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LONGERON 23L BS 1297 TO 1323. REPAIRED IAW SRM 53-02-F16.

Part: PAN — CRACKED (CARGO DOOR) · airframe 61,052 hrs · 45,613 cycles

CRACKED INNER PAN ON AFT CARGO COMPARTMENT DOOR INNER STRUCTURE OF AFT EDGE BTW UPPER EDGE AND BEAM NR 5. PAN WAS REPAIRED IAW ER/A 455904-14MA REV A ASSOCIATED ER/A 45-590414 ADDED FOR AC 0938.

Part: SUPPORT — BROKEN (BS 237-256) · airframe 61,052 hrs · 45,613 cycles

BROKEN SLANT PANEL SUPPORTS BS 237 AND 256. PANEL SUPPORTS REPLACED IAW E/A 413029-14 MA REV.

Part: SEAT TRACK — CORRODED (BS 1136-1160) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON SEAT TRACK X=44 FROM BS 1136 TO 1160. SEAT TRACK REPLACED IAW SRM 53-05, FIG YF.

Part: SUPPORT — CORRODED (BULKHEAD) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LOWER SUPPORT OF AFT BULKHEAD BETWEEN 24RH TO 24LH AT MID CARGO COMPARTMENT. REPAIR DOUBLER WAS INSTALLED IAW SRM 53-01, FIG 2, (SHEET 3).

Part: LONGERON — CRACKED (FUSELAGE) · airframe 61,052 hrs · 45,613 cycles

CRACKED LONGERONS 3 LT AT INTERSECTION WITH FRAME Y=1437 AFT ACCESSORY COMP. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: SKIN — DAMAGED (BS 579-598) · airframe 61,218 hrs · 45,747 cycles

A LIGHTNING STRIKE WAS REPORTED ON THE RT WINDOW BELT PANEL BETWEEN BS 579 AND 598. A REPAIR DOUBLER WAS INSTALLED.

Part: LONGERON — CRACKED (BS 1212 L4R) · airframe 61,052 hrs · 45,613 cycles

CRACK ON LONGERON NR 4 RT AT STA Y=1212 CABIN STRUCTURE. LONGERON WAS REPAIR IAW SRM 53-02, FIG 18, RII COMPLETED.

Part: INTERCOSTAL — CORRODED (FUSELAGE) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON INTERCOSTAL. FOUND OUT OF LIMITS IAW DWG 9915563, REV F, AW 9919661, REV B.

Part: TEE FITTING — CORRODED (BS 1380) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LOWER TEE CAP BS 1380, BETWEEN X=20 TO X=-12. REPLACED IAW DWG 9912246, REV DE AND CE.

Part: SEAT TRACK — CORRODED (BS 432-632) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON RT SEAT TRACK X=-54 BTW BS 432 TO 632. CORROSION OUT LIMITS, REPAIRED IAW SRM 53-05, FIG 4A AND ER/A 485415-14 MA.

Part: BEAM — CORRODED (FUSELAGE) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LOWER DOOR FRAME BEAM AT MID CARGO COMPARTMENT BS 636-693. CORROSION WAS REMOVED IAW SRM 51-10-3, PAR 26. AREAS WITHIN LIMITS WERE TREATED AND PRINTED IAW SRM 51-10.

Part: RIB — CORRODED (LT WING SLAT) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON INBD RIB BOTH FACE XOS= 580.519 AT LT WING SLAT PANEL NR 5 (LW) (AWR) REF NRC (T0 262730) RIB WAS REPLACED IAW DWG. 593763 REV: AH AND SRM 51-30-2, 51-30-8.

Part: LONGERON — CRACKED (BS 1309 L5L) · airframe 61,052 hrs · 45,613 cycles

CRACK ON LONGERON 5L BS 1309 AT CABIN STRUCTURE. LONGERON REPAIRED IAW SRM 53-02, FIG 18.

Part: FITTING — CORRODED (BS 1322 L29L) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON FRAME CLIP AT BS 1322 LONG 29L AFT CARGO COMPARTMENT. FRAME CLIP AREA OUT LIMITS WAS REMOVED, FABRICATED, AND INSTALLED IAW SRM 53-03D, FIG 3.

Part: LONGERON — CRACKED (BS 845 L3R) · airframe 61,052 hrs · 45,613 cycles

CRACK ON LONGERON 3RT AT BS 845. REPAIRED IAW SRM 53-02, FIG 18.

Part: FLOORBEAM — CORRODED (CORRODED) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON BS 712 TO 840 BETWEE STA X=-54 TO -60 AT CABIN FLOOR STRUCTURE. REPAIRED IAW ER/A 398191-14 MA, REV B.

Part: LONGERON — CRACKED (BS 1437 L16L) · airframe 61,052 hrs · 45,613 cycles

CRACKED LONGERON 16L BS 1437. LONGERON REPLACED IAW DWG 5910228, REV KF.

Part: SEAT TRACK — PUNCTURED (BS 200-256) · airframe 61,052 hrs · 45,613 cycles

PUNCTURES ON SETTLEMENT AREA AT SEAT TRACK X=44 BTW BS 200 TO 256 AT CABIN FLOOR STRUCTURE (CFS). REF NRC (T0 262836) SEAT TRACK SECTION WAS REPLACED IAW SRM 53-05, FIG 4F.

Part: LONGERON — CRACKED (BS 655 L2R) · airframe 61,052 hrs · 45,613 cycles

CRACKED LONGERON 2RT STA Y=655 AT FUSELAGE INTERNAL STRUCTURE (F/S) (REF NRC:T0 263597) SECTION LONGERON WAS REPLACED IAW 53-02 RII COMPLETED.

Part: SEAT TRACK — CORRODED (BS 454-611) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LT SEAT TRACK X=54 REPAIR PLUGS STA Y=454-457 Y=577-582 AND Y=607-611 AT FLOOR CABIN ESTRUCTURE IN REF NRC OM828H CARD 47 ZONE 58 AND (T0 262795) (FCS). REF NRC (T0 263825) REPAIR PLUGS WERE REPLACED IAW SRM 53-05, FIG 4A AND 51-30-1.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION OUT OF LIMITS ON (2EA) COUNTERSINK AT RT WING FUEL TANK ACCESS PLATE NR 1414C IN REF NRC OM828D NR 148, ZONE 14 AND (T0 263703) REF NRC: (T0 263748) ACCESS PLATE 1414C 2 EA COUNTERSINK WERE REWORKED, REPAIR BUSHINGS WERE FABRICATED AND 2 E/A REPAIR BUSHINGS WERE INSTALLED IAW SRM 51-22-2A CONDITION II.

Part: CUSP WEB — CORRODED (BS 288) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON RT CUSP WEB UPPER AND LOWER SURFACE STA Y=288 X=-54 TO X=-60 AT FLOOR CABIN STRUCTURE. IN REF. RT CUSP WEB STA Y=288 X=-54 TO X=-60 AT FLOOR CABIN STRUCTURE WAS REPAIRED IAW SRM 53-05, FIG 13/A-13.

Part: ACCESS DOOR — CORRODED (FUEL) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON COUNTERSINK OF LT WING FUEL ACCESS PLATE NR 1379C, REF OM828C ACCESS PLATE NR 1379C 1EA CONUNTERSINK WAS REMOVED, REPAIR BUSHINGS WERE FABRICATED, AND 1/A REPAIR BUSHING WAS INSTALLED IAW SRM 51-22-2A CONDITION II.

Part: ACCESS PANEL — CORRODED (RT WING) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON COUNTERSINK (16EA) AND SETTELEMENT AREA OF RT WING FUEL ACCESS PLATE NR 1460C, REF OM828D CARD 25 ( REF NRC: (T0 263624) FUEL ACCESS NBR 1460C WAS REPLACED IAW SRM 5122-2A.

Part: LONGERON — CRACKED (BS 1289 L9L) · airframe 61,052 hrs · 45,613 cycles

CRACK ON LONGERON NBR 9LT STA Y=1289 CABIN STRUCTURE (C/C) REF (T0 263117). LONGERON WAS REPAIRED IAW 53-02 FIG. 18.

Part: LONGERON — CRACKED (BS 160 L3L) · airframe 61,052 hrs · 45,613 cycles

CRACKED LONGERON 3 LT STA Y=160 OF PAX CABIN INTERNAL STRUCTURE: LONGERON 3 LT WAS REPLACED IAW SRM 53-02, FIG 18.

Part: ACCESS DOOR — CORRODED (FUEL) · corrosion level 2 · airframe 61,052 hrs · 45,613 cycles

CORROSION ON COUNTERSINKS AND SETTLEMENT AREA OF LT WING FUEL ACCESS PLATE NR 1357C. FUEL ACCESS PLATE NR 1357C WAS REPLACED.

Part: LONGERON — CORRODED (BS 1257-1290) · airframe 61,052 hrs · 45,613 cycles

CORROSION ON LONGERON 22 LT, BS 1257 AND 1290 AT AFT CARGO COMPARTMENT REPAIRED IAW SRM 53-02, FIG 18 AND DWG 59 3602 REV EH.

Part: TAB — DENTED (LT ELEVATOR) · airframe 61,053 hrs · 45,614 cycles

DENTS ON LT ELEVATOR ANTI-FLOAT TAB UPPER SURFACE (20 EA) REF NRC DAMAGE OUT OF LIMITS FOR REPAIR IAW SRM 55-04, PARA 2C. REPLACED IAW SRM 55-20.

Part: TAB — DENTED (LT ELEVATOR) · airframe 61,053 hrs · 45,614 cycles

DENTS ON LT ELEVATOR CONTROL TAB UPPER SURFACE. DAMAGE OUT OF LIMITS FOR REPAIR IAW SRM 55-04, PARA 2C LT ELEVATOR CONTROL TAB WAS REPLACED IAW SRM 55-20.

Part: SKIN — DAMAGED (BS 579-589) · airframe 61,052 hrs · 45,613 cycles

LIGHTNING STRIKE ON RT WINDOW BELT FRAME BTW STA Y=579-598 FWD UPPER CORNER. REPAIR WAS ACCOMPLISHED IAW ER/A 506660-14 REV ORIG.

Part: SKIN — DAMAGED (BS 579-598) · airframe 61,052 hrs · 45,613 cycles

LIGHTNING STRIKES ON LT WINDOW BELT FRAME BTW BS 579-598 FWD AND AFT EDGES. REPAIR WAS ACCOMPLISHED IAW ER/A 506661-14 REV ORIG.

Part: UNKNOWN — SMOKE (CABIN) · airframe 60,052 hrs · 44,922 cycles

THE CREW DIVERTED THE AIRCRAFT TO JFK AFTER THE FLIGHT ATTENDANTS REPORTED VISIBLE SMOKE AND AN ODOR OF BURNING PLASTIC IN THE CABIN. MAINTENANCE WAS NOT ABLE TO DUPLICATE THE SMOKE AND FOUND NO OTHER DISCREPANCIES. VISUAL INSPECTION AND A 20 MINUTE PACK BURN-OUT WERE PERFORMED WITH NO TROUBLE FOUND. AIRCRAFT HAS RETURNED TO SERVICE.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

RE-WRITE FROM NR 108 SUPPORT ANGLE HAS CORROSION BETWEEN STA 1307-1338 RBL 17. REMOVED CORROSION, FOUND TO BE OUT OF LIMITS. INSTALLED NEW SUPPORT ANGLE IAW DC-9/MD88 SRM 51-30. DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: SUPPORT ANGLE — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

RE-WRITE FROM N/R 109, AREA 8-0 SUPPORT ANGLE HAS CORROSION BETWEEN STA 1307-1338 LBL 17. SUPPORT ANGLE FOUND TO BE OUT OF LIMITS PER DC-9/MD88 SRM 53-01 FIG 1. REMOVED SUPPORT AND INSTALLED NEW PER MD88 SRM 51-30 DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: WINDOW FRAME — CRACKED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

PAX CABIN LT WINDOW FRAME FS 1174-1193 INTERNAL DOUBLER CHANNEL CRACKED AT UPPER AFT CORNER. REMOVED AND REPLACED INTERNAL DOUBLER RING IZW DC-9/MD88 SRM 51-30 DURING PAX MOD VISIT ST AEROSPACE SAN ANTONIO.

Part: INTERCOSTAL — DAMAGED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

MAIN CABIN RIGHT SIDE INTERCOSTAL HAS MIS DRILLED HOLES AT FS 243 AND 245 ON LONGERON L9R SAA102- DAMAGE MAIN CABIN RT. SUBMITTED TO ENGINEERING.AT SAA/SAT DURING PAX MOD. DOCUMENTED ON N/R 110 W/O 89247320001.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

FLOOR SUPPORT CHANNEL STA 200 BETWEEN LBL 8 AND RBL 8 HAS CORROSION. FLOOR SUPPORT CHANNEL FOUND TO BE OUT OF LIMITS PER DC-9/MD80 SRM 51-10-3. REMOVED, FABRICTED AND INSTALLED NEW FLOOR SUPPORT CHANNEL DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

SEAT TRACK HAS AREAS OF CORROSION STA 1079 TO 1314 LBL 24. EXFOLIATION ON SEAT TRACK FOUND TO BE OUT OF LIMITS PER DC-9/MD80 SRM 53-05. REMOVED SEAT TRACK AT ACTUAL LOCATION LBL 22 FROM STA 1088-1314, INSTALLED NEW SEAT TRACK AND SPLICE IAW MD88 SRM 51-30-50 DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

FLOOR SUPPORT CHANNEL HAS CORROSION STA 160-200 RBL 48. MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER MD80/DC-9 SRM 53-01. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL DURING PAX MOD AT ST AEROSPACE SAN ANTONIO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

TRACK CHANNEL HAS AREAS OF CORROSION STA 1098 TO 1214 AT BL-0 CORROSION EXCEEDS LIMITS PER MD88 SRM 53-01. TRACK CHANNEL REPLACED PER PAX MOD EA 09-482472 STEP 6 DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: SUPPORT CHANNEL — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

THRESHOLD SUPPORT CHANNEL AND MEMBRANE HAS CORROSION EXTENDING UNDER L-1 DOOR THRESHOLD PLATE. MEMBRANE MATERIAL LOSS WITHIN LIMITS, SUPPORT CHANNEL MATERIAL LOSS OUT OF LIMITS PER MD88 SRM 51-01. FABRICATED NEW SUPPORT CHANNEL AND INSTALLED DURING PAX MOD VISIT.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

FLOOR SUPPORT CHANNEL HAS CORROSION STA 200 BETWEEN RBL 0 AND RBL 48. SUPPORT CHANNEL FOUND TO BE OUT OF LIMITS PER DC-9/MD-88 SRM 53-01. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT CHANNEL DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: FLOOR SUPPORT — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

FLOOR SUPPORT ANGLE HAS CORROSION STA 160 TO 200 LBL 48. MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER MD80/DC9 SRM 53-01. REMOVED, FABRICATED AND INSTALLED FLOOR SUPPORT DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: SEAT TRACK — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

SEAT TRACK HAS CORROSION STA 200-313 LBL 48. REMOVED AND REPLACED SEAT TRACK SECTION FROM FS 200-305 LBL 48 DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: CHANNEL — CORRODED (FUSELAGE) · airframe 59,058 hrs · 44,239 cycles

TRACK CHANNEL HAS CORROSION STA 148-200 RBL 7. MATERIAL LOSS FOUND TO BE OUT OF LIMITS PER DC9/MD80 SRM 51-01. REMOVED CHANNEL, FABRICATED AND INSTALLED TRACK CHANNEL DURING PAX MOD VISIT AT ST AEROSPACE SAN ANTONIO.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 59,008 hrs · 44,214 cycles

PASSENGER SEAT 24E EMERGENCY FLOOR LIGHTING INOPERATIVE. RE-TERMINATED CONNECTOR AT SEAT 24E. LIGHTS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (EXTERIOR) · airframe 58,665 hrs · 43,953 cycles

DURING A LAYOVER CHECK, MAINTENANCE FOUND THE DOOR 4L AND DOOR 4R EXTERIOR EMERGENCY LIGHTS INOPERATIVE. MAINTENANCE RE-SECURED THE LIGHT ASSEMBLIES. OPERATIONAL CHECKS WERE GOOD.

Part: CONNECTOR — DEFECTIVE (CABIN) · airframe 58,614 hrs · 43,915 cycles

DURING LINE CHECK MAINTENANCE FOUND EMERGENCY LIGHTS AT SEATS 11 AND 18 INOPERATIVE. MAINTENANCE TERMINATED CONNECTORS PER SWPM. OPERATION OF LIGHTS CHECKS OK.

Part: BALLAST — FAULTY (CABIN) · airframe 58,283 hrs · 43,667 cycles

SMOKE AND BURNING ELECTRICAL SMELL ORIGINATING FROM OVERHEAD BIN AREA AROUND ROW 29 TO REAR OF CABIN. MAINTENANCE FOUND FORWARD BALLAST ROW 27ABC FOR LOWER SIDEWALL LIGHTS TO BE INOPERATIVE. BALLASTS WERE REPLACED AT ROW 24ABC AND 27ABC. OPERATED CABIN LIGHTS WITH SEVERAL POWER CHANGES AND ALL CHECKS WERE GOOD. NO FURTHER TROUBLE, SMOKE, OR SMELL.

Part: SKIN — DENTED (FUSELAGE) · airframe 53,345 hrs · 40,363 cycles

DENTS ON FUSELAGE SKIN ON STA Y=446 TO 454 BETWEEN LONGS 25-28 RT. DENTS FOUND OUT OF LIMITS IAW SRM 53-04D FIG 12C. NO CRACKS NOTED. REPAIR PARTS FABRICATED AND INSTALLED IAW SRM 53-04D FIG 12C.

Part: SKIN — DAMAGED (FUSELAGE) · airframe 53,229 hrs · 40,279 cycles

FAA FINDING: DENT WITH CREASE AT FS 237 ABOUT LONG 17L. DAMAGE WAS REMOVED, REPAIR ITEMS FABRICATED AND INSTALLED IAW SRM 53-04D FIG 12B.

Part: BEAM — CORRODED (CARGO BAY) · airframe 53,207 hrs · 40,266 cycles

EXFOLIATION CORROSION ON C2 CARGO COMP DOOR JAMB LOWER BEAM BETWEEN STA Y=636 T0 Y=693. REMOVED CORROSION IAW SRM 51-10-3 PAR 35. REPAIR PARTS WERE FABRICATED AND INSTALLED IAW SRM 53-05 FIG 123.

Part: SUPPORT FITTING — DAMAGED (RT MLG) · airframe 53,176 hrs · 40,247 cycles

TOOLING MARKS ON RT MLG SUPPORT FITTING BEARING BORE. BEARING BORE WAS CLEANED UP IAW DWG SR09570087 AND EA 09-093855-03AD 0204. NO CRACKS FOUND IAW 09-093855-03AD 0104.

Part: ACM — LEAKING (NR 1) · airframe 50,435 hrs · 38,458 cycles

FLOW LIGHT ON CLIMB-OUT PASSING FL280. BOTH AC PACKS ON. NO AUTO PRESS INOP LIGHTS ON. C/W QRH PROCEDURES NO HELP. CLOSED OUTFLOW VALVE, NO HELP. BOTH PNEU X FEED VALVES CLOSED. FOUND 1 LEAK AT RT ACM 1 LEAK FROM HEAT EXCHANGE ON LEFT SIDE ON 1 OPEN DUCT ON HOT AIR SUPPLY LINE THE SPIDER DUCT FIXED ALL 3 LEAKS LEAK CHECK OK.

Part: FASTENER — LOOSE (FUSELAGE) · airframe 47,175 hrs · 36,396 cycles

FUSELAGE SKIN REPAIR BETWEEN STA 560-588 AND LONGERONS 22-26R - LOOSE FASTENERS ON PREVIOUS REPAIRS. SKIN REPAIRED PER DRAWING AMR0953589 AND APPROVED BY ERA 460134-14.

Part: SKIN — CORRODED (FUSELAGE) · airframe 46,965 hrs · 36,244 cycles

THE FUSELAGE SKIN WAS CORRODED FROM FS 564 TO 588, L22R-L26R. THE DAMAGED FUSELAGE SKIN WAS CUT OUT AND A REPAIR DOUBLER WAS INSTALLED.

Part: DOOR FRAME — CRACKED (FUSELAGE) · airframe 46,965 hrs · 36,244 cycles

FWD SERVICE DOOR JAMB REPAIR - CRACK AT FWD UPPER CORNER OF FWD SERVICE DOOR JAMB STA 173. PERMANENT REPAIR INSTALLED PER SRM 53-05D FIGURE 112.

Part: SKIN — DELAMINATED (T/E FLAP VANE) · airframe 46,965 hrs · 36,244 cycles

OUTBOARD FLAP INBD GUIDE VANE REPAIR - DELAMINATION ON LEFT OUTBOARD FLAP INBOARD GUIDE VANE LEADING EDGE. PERMANENT REPAIR INSTALLED SRM 37-03D, PARA 8A, FIG 9A.

Part: SKIN — DENTED (FUSELAGE) · airframe 46,965 hrs · 36,244 cycles

FUSELAGE SKIN REPAIR AT STA 222 BETWEEN LONGERONS 15L AND 17L - SKIN DENTED. INSTALLED PERMANENT REPAIR PER SRM 53-04D, FIG 12B.

Part: FRAME — CRACKED (FS 864) · airframe 46,965 hrs · 36,244 cycles

DURING HMV-3 A CRACK WAS FOUND IN THE FS 864 RT OVERWING FRAME JUST BELOW THE FLOOR LINE. A NEW FRAME WAS INSTALLED PERS/B MD80-53A301.

Part: ATTACH ANGLE — CRACKED (FUSELAGE) · airframe 41,805 hrs · 32,619 cycles

FS 1422 VERTICAL STAB TO FUSELAGE INTERFACE: CRACK REPAIR. THE LT AND RT ATTACH ANGLES FOR THE INTERFACE BETWEEN THE VERTICAL STABILIZER AND THE FUSELAGE WERE FOUND CRACKED. THE UNDERLYING SKIN ON THE RT SIDE AT FS 1422 WAS ALSO FOUND CRACKED. THE ANGLES WERE REPAIRED PER DAC S/B DC9-53-223 AND THE SKIN WAS REPAIRED WITH A TITANIUM DOUBLER PER ER/A 096670-14AD.

Part: WEB — CORRODED (FUSELAGE) · airframe 38,690 hrs · 30,466 cycles

CORROSION ON RIGHT CUSP WEB AT STATION Y=579. REPLACED DAMAGED SECTION OF RIGHT CUSP WEB FROM STA 560 TO STA 598 PER DELTA DRD 53-20-02D PAGE 801 DUE TO CORROSION OUT OF LIMITS AT STA 578.

Part: BLADE — DAMAGED (NR 1 ENGINE) · airframe 37,090 hrs · 29,324 cycles

AFTER TAKEOFF, GSO LEFT ENGINE INGESTED LARGE BIRD. MANY BLADES BENT AND AT LEAST ONE MIDSPAN SHROUD BROKEN OFF. REPLACING ENGINE.

Part: ENGINE — FAILED (NR 2) · airframe 36,385 hrs · 28,857 cycles

DURING CLIMB THRU FL 240 ENG A/I ON RT ENGINE FAILED N2 0 OIL PRESSURE 0, HYD PRESSURE 0, DISCHARGED FIRE BOTTLE INTO RT ENGINE. REPLACED NR 2 ENGINE

Part: ODOR — DETECTED (CABIN/COCKPIT) · airframe 36,297 hrs · 28,803 cycles

DURING TAKEOFF FLT ATTENDANT REPORTED AN ODOR THROUGHOUT THE CABIN. ODOR WAS EVIDENT ALSO IN COCKPIT. NO ALARMS, NO VIVIBLE SMOKE. CHECKED GALLEYS, NOTHING CAUSING ODOR. APU WAS OFF CROSSFEED CLOSED AND ENGINES AT CLIMB EPR. ODOR DISSAPATED AT 15000 FT AND WAS GONE BY FL310. PERFORMED DUCT BURNOUT.

Part: BALLAST — OVERHEATED (CABIN) · airframe 35,115 hrs · 28,007 cycles

WHITE SMOKE CAME FROM OVERHEAD BIN, FROM A RECESSED PANEL IN OVERHEAD BIN. POWER WAS REMOVED FROM AIRCRAFT. PERFORMED OPS 5088. FOUND OVERHEAD CEILING LIGHT BALLAST OVERHEATED. REPLACED BALLAST. ELECTRICAL PIGTAIL BAD. REPLACED SAME.

Part: GENERATOR — MALFUNCTIONED (RT ENGINE) · airframe 34,973 hrs · 27,910 cycles

DIVERSION, RT A/C SYSTEM BUS FAILURE. COULD NOT PWR FROM OTHER SOURCES. FOUND DISTURB FAULT ON GCU AND CROSSTIE LOCKOUT ON EOAP INSP GEN FEEDER CABLES FROM GEN TO TAIL SECTION, CKS OK. MEGGED GEN CABLES, CKS OK. REMOVED AND REPLACED NR 2 CTS, 3 EACH AND GEN AND GCU PER MM RAN ENG CKS OK.

Part: SMOKE — DETECTED (CABIN) · airframe 33,828 hrs · 27,026 cycles

AT FL270 F/A NOTIFIED US OF SMOKE /FUMES /STRONG BURNING ODOR. SMOKE PREVALENT AT OVERWING EXITS ROW 24 TO 27. ODOR MOVED FORWARD TO COCKPIT. SMOKE COMING OUT OF ALL AIR VENTS IN MAIN AND FIRST CLASS CABIN. CABIN FULL OF SMOKE FOR 3-5 MINS. C/W STEPS 1-4 OF OPN 5088 BORESCOPED NR 1 AND 2 ENGINES NR 3 CARBON SEAL. NO LEAKS FOUND. COMPLETED OPN 5088, NO EVIDENCE OF SMOKE OR FUMES DURING OPN 5088. PERFORMED VERIFICATION FLT, NO ABNORMALITIES.

Part: ENGINE — MALFUNCTIONED (NR 1) · airframe 32,892 hrs · 26,327 cycles

AT 1000 FT AGL ENG ROLLED BACK TO 4-5 N1. NOISE AND VIBE WAS FELT THROUGH ENTIRE A/C. 2 MINS LATER WITH MINIMAL INDICATIONS, OIL PRESSURE WAS LOST AND ENGINE WAS SHUTDOWN. ACFT ARRIVED AT DNTC WHERE NR 1 ENG WAS REMOVED AND REPLACED WITH ENG SERIAL 725998.

Part: TURBINE — DAMAGED (NR 2 ENGINE) · airframe 32,616 hrs · 26,128 cycles

CLIMBING THROUGH 22,000 FT, RIGHT ENGINE BANGED AND NOTED EGT DECREASING THROUGH 650 DEG C WITH INDICATIONS THAT ENGINE WAS ROLLING BACK. ENGINE SHUT DOWN AND RETURNED TO ATL. FOUND TURBINE SECTION DAMAGED. REPLACED ENGINE.

Part: ENGINE — STALLED (NR 1) · airframe 31,916 hrs · 25,615 cycles

AT FL 290 HAD WHAT APPEARED TO BE COMPRESSOR STALL IN LT ENGINE EPR DECREASED AND RAPIDLY INCREASE BACK TO NORMAL. FELT HARD JOLT MOMENTARY OFF FLAG IN STBY ADI. SMELL OF RUBBER BURNING. FELT SLIGHT VIBRATION FOR REMAINDER OF FLT. FOUND NR 1 ENG FAN BLADE DAMAGE, 1 WITH TEAR AND 6 OTHER BLADES BENT. C/W BORO OF 6/7-5/6 COMPRESSOR AND 1/2/5/6, TURBINE BLADES PER M/M 72-33-21-8. NO DISCREPANCIES FOUND. ITEM FOR BLADE DISCREPANCIES TRANSFERRED TO ITEM 4. REPLACED BLADES.

Part: HOUSING — CHAFED (NR 2 ENGINE) · airframe 30,497 hrs · 24,577 cycles

A/C 938 WAS IN THE PROCESS OF HAVING A NR 2 ENGINE CHANGE. AT THAT TIME THE AIRCRAFT CASE DRAIN FILTERS WERE ALSO CHANGED. THE MECHANIC REPLACING THE FILTERS NOTICED A CHAFED AREA AND BURNT SPOT ON THE CASE DRAIN FILTER HOUSING CAUSED BY THE NR 2 ENGINE GENERATOR FEEDER CABLES. THE FILTER HOUSING WAS REPLACED ALONG WITH THE GENERATOR FEEDER CABLES.

Part: RIB — WORN (WS 112)

RIB DAMAGED FROM CABLE AT L/E STA FS 123. RIB WORN THRU AT L/E WIND STATION FS 112 FROM CABLE. L/E FITTING DAMAGED FROM CABLE AT STA FS 135 APPROX .5 INCH. RIB DAMAGED FROM CABLE AT L/E STA FS 129. L/E FITTING DAMAGED FROM CABLE AT STA FS 140 APROX .25 INCH. ALL REPAIRED PER APPROVED MANUALS.

Part: LIGHT — INOPERATIVE (CABIN)

MID ATTENDANT FLASHLIGHT NOT BLINKING. REPLACED FLASHLIGHT, CKS GOOD.

Part: PRESSURE SYST — MALFUNCTIONED (CABIN)

ON CLIMB-OUT, LOST CABIN PRESSURE, THE PACKS OVER TEMPED AND SHUT OFF. THE A/C DECREASED ALT AND RETURNED TO PHX. FOUND NO DUCT LEAKS. BOTH PACKS OPERATED NORMAL. PRESSURIZEDTO 5 PSID WITH EACH PACK, THEN WITH BOTH PACKS. REPAIRED THE A/C FOR FERRY FLT TO DFW FOR OXY CANISTER MTC.

Part: BATTERY PACK — DISCHARGED (CABIN)

ON LAYOVER, NR 2 CHECK FOUND EMERGENCY TRACK LIGHTING ON FLOOR IN AFT OF A/C INOP. BORROWED EMERGENCY TRACK LIGHTING BATTERY PACK FROM TWA (S/N 30). INSTLD PACK IN EMERGENCY BATTERY PACK POSITION IN OVERHEAD BIN ABOVE SEAT 37DE. ALL EMERGENCY TRACK LIGHTING OPS CHK NML AT THIS TIME.

Part: SKIN — DENTED (FS 229-266)

LEFT FUSELAGE SKIN WAS DENTED AND PREVIOUSLY REPAIRED. DURING HMV, THE REPAIR WAS REMOVED AND ADDITIONAL DAMAGE WAS FOUND RESULTING IN AN ENLARGED CUTOUT. SINCE THE DAMAGE IS NEAR THE PANEL FOWARD END, THE FORWARD SECTION OF THE SKIN PANEL IS CUT VERTICALLY AT FS 266 FROM THE LOWER EDGE OF THE PANEL AT THE CUSP STRINGER 18L UP TO THE PANEL UPPER EDGE BELOW STRINGER 15. THE FORWARD SECTION OF THE PANEL EXTENDING FROM FS 229 AFT TO FS 266 CONTAINING THE DAMAGE IS REMOVED AND REPLACED, AND A REPAIR ADDED AT FS 266. ACCOMPLISHED REPAIRS PER DL ERA 273434-14, REV A.

Part: DOOR JAMB — DAMAGED (FWD SERVICE DOOR)

FUSELAGE FWD SERVICE DOOR SURROUND STRUCTURE LOWER JAMB PAN WAS DAMAGED BY TOOLING. THE DAMAGE CONSISTS OF PUNCTURES COMPLETELY THROUGH THE PAN AT BOTH THE FWD AND AFT LOWER CORNERS, REQUIRING REPLACEMENT. A REPLACEMENT PAN IS NOT IMMEDIATELY AVAILABLE, SO THE REPAIR CONSISTS OF SPLICING IN REFABRICATED REPLACEMENT SECTIONS PER THE MD-88 SRM WILL BE ACCOMPLISHED REF DL ERA 273424-14 REV B.

Part: JAMB PAN — PUNCTURED (SERVICE DOOR)

THE FUSELAGE FORWARD SERVICE DOOR SURROUND STRUCTURE LOWER JAMB PAN WAS DAMAGED FROM TOOLING. THE PAN HAS SEVERAL PUNCTURES. REPLACEMENT PAN IS NOT AVAILABLE, SO FABRICATED SECTION WAS SPLICED IN PER THE MD-88 SRM, REFERENCE DL ERA 273424-14.

Part: PACK — INOPERATIVE (LEFT)

AFTER TAKEOFF, A/C WOULD NOT PRESSURIZE, LEFT PACK SUPPLY WAS ZERO. FLT ATTENDANT REPORTED LOUD SOUND LEFT AFT DOOR, OAP SHOWED NO DOOR LIGHTS. PERFORMED POM PROCEDURE, NO EFFECT. FOUND BOTH PACKS INOP, RT PACK INTERMITTENT OPERATION. FWD RT PACK TO MCO/PLAC REF MEL 21-00-01A, REPLACED THERMAL SWT 190F FOR LEFT A/C SYS, PACK CHECKS GOOD. BORROWED SWT FROM RT SYS (P/N 219101528).

Part: SKIN — DAMAGED (BS 541-560)

DURING ROUGH WEATHER AT BDL, AN AIR STAIR CART COLLIDED WITH THE FUSELAGE AND LEFT A 4 INCH BY 9 INCH HOLE. ALSO, DAMAGING LONGERON 20L, BETWEEN FS 541 AND 560.

Part: FRAME — CRACKED (RT MLG WW)

FOUND ON F2 LETTER CK, FORWARD OUTBD FRAME OF RT W/W OPENING IS CRACKED 2 INCHES. REPAIRED PER SRM 53-05.

Part: LINK — WORN (NLG DOOR)

AFTER TAKOFF AND GEAR RETRACTION, HAD LOUD WIND NOISE FROM NOSE WHEELWELL AREA. NO OTHER ABNORMAL INDICATIONS WERE NOTED, RETURNED TO COS. FOUND LEFT NOSE GEAR DOOR OPEN, FOUND WORN DOOR LINK. REPLACED LINK, OPERATION NORMAL.

Part: TE SKIN — DELAMINATED (ELEVATOR TAB)

AT HMV, ELEVATOR TAB WAS FOUND WITH DAMAGE ON TRAILING EDGE AT 8 INCHES FROM O/B END. REPAIRED PER SRM 55-04.

Part: FRAME — CRACKED (LT MLG WW)

TWO INCH CRACK ON LEFT W/W CUT-OUT ON GL OUTBOARD END LEFT WING. ITEM FOUND DURING F-1 LETTER CHECK. REPAIRED PER SRM 53-05-FIG 81A.