N938DN
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| DELTA AIR LINES, INC. (DALA) | Operator | 2017-09-04 – 2017-09-04 | Operator named in NTSB report |
| DELTA AIR LINES INC | Operator | 2017-09-04 – 2017-09-04 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
NR 1 ENGINE UPPER PYLON APRON CENTER SECTION MISSING AND AFT SECTION DAMAGED. R & R THE PYLON APRON CENTER AND AFT SECTIONS .
OVERWING EMERGENCY EXIT LIGHTS DID NOT ILLUMINATE, LOWER INTERIOR EXIT SIGNS. REMOVED AND REPLACED THE BATTERY PACK IAW AMM 33-55-03. OK FOR SERVICE.
TAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 2 CLOCK POSITION IS CRACKED AT INR T-CHORD. REPAIRED STA 1520 CANTED BULKHEAD FRAME PRI 569819-14AD REV 0 AND ERA 569819-14AD REV ORIGINAL SECTION I.
SUB FLOOR UNDER FLOOR BOARDS 221GF AND 221HF IS IN CORRODED AT FASTENER HOLES BETWEEN STA 168 AND STA 200. REPAIRED W/ REF TO PRI 570298-14, REV 0; PRI 570298-14, REV 1 AND ERA 570298-14, REV ORIG.
ERA 569819-14 SECTION I ISSUED FOR REPAIR TO STA 1520 NEAR L7R. REPAIRED STA 1520 CANTED BULKHEAD FRAME REF PRI 569819-14AD REV ORIGINAL.
TAIL INTERIOR CANTED FRAME CBS 1520 AFT WEB NEAR 10 CLOCK POSITION IS CRACKED AT INNER T-CHORD. REPAIRED WEB REF SRM 53-10-03 FIG 9C.
LEFT SIDE FUSELAGE APPROXIMATE LOCATION FRAME 1496 BETWEEN STRINGER 3 AND 4. TWO CRACK INDICATION WITH BAY MARKED. REPAIRED PER PRI 570252-14 REV 0,1,2 AND ERA 570252-14 REV ORIGINAL.
EMERGENCY EXIT LIGHT AT ROW 27 INOPERATIVE ON BOTH SIDES. SECURED TERMINAL LUG AT S3-554, STA 1126R. OPERATION CHECKS GOOD.
EMERGENCY EXIT COVER DIFFUSER LENS DAMAGED ON OR MISSING. REPLACED LENS OPERATION CHECKS GOOD.
EMERGENCY FLOOR LIGHTING DAMAGED. SECURED LIGHT STRIP. OPERATION CHECKS GOOD.
LEFT AFT OVERWING EXIT SIGN AND RIGHT AFT OVERWING EXIT SIGN INOPERATIVE. REPLACED THE BATTERY PACKS.
TAIL CONE SKIN DENTED. COMPLIED WITH PRI 540706-14, REV B, REVISION 0, 1, & 2 IAW ERA 540706-14, REV B.
EMERGENCY EXIT LENS COVER MISSING AT DOOR 1R. INSTALLED NEW EMER EXIT LENS COVER.
L1 DOOR SLIDE UNSECURED. REMOVED AND REPLACED IAW MM.
EXIT SIGN COVER OVER CABIN MAIN ENTRANCE DOOR KEEPS FALLING DOWN. SECURED THE COVER. (LP# 9461452)
EMERGENCY EXIT SIGN COVER LOOSE. RE INSTALLED COVER.
EMERGENCY FLOOR LIGHTING INOPERATIVE. RESECURED 17A - 20A FLOOR LIGHTING. OKAY FOR SERVICE.
AIRCRAFT SKIN HAS CRACK AT BS 1437. REPAIRED IAW PRI/ERA 549478-14.
FUSELAGE SKIN CRACKED AT NOSE WHEEL WELL AFT DOOR HINGE CUTOUT. REPAIRED IAW SRM 53-30-01.
VERTICAL STABILIZER LEADING EDGE LOWER RIGHT INNER ATTACH ANGLE BROKEN. REPLACED THE ATTACH ANGLE IAW DWG 5912188.
VERTICAL STABILIZER LOWER LEFT INNER ATTACH ANGLE IS BROKEN. REPLACED IAW DWG 5912188.
L1 DOOR THRESHOLD STRIP CORRODED. REPLACED IAW SRM 51-30-00.
CAPTAIN'S SLIDING WINDOW FRAME CRACKED AT UPPER AFT CORNER. REPAIRED IAW DWG 5911356 AND 5644324 AND PRI/ERA 549506-14.
LONGERON 2R CRACKED AT BS 1475. REPAIRED IAW SRM 53-30-01, FIG 14.
FLIGHT CREW REPORTS SPARKS WHILE MOVING CAPTAIN'S LIGHT. CIRCUIT BREAKER TRIPPED AND WAS NOT RESET. INSTALLED NEW LIGHT. OPS CHECKED GOOD.
DAMAGE TO L1 DOOR LOWER LT CORNER FLANGE. REPAIRED DAMAGE IAW SRM 52-01-01.
UPPER CANTED FRAME AT BS 1567.407 DAMAGED. REMOVED, FABRICATED AND INSTALLED FRAME IAW DWG 9911843.
DECLARED AN EMERGENCY ON APPROACH DUE TO RT HYD SYS LOW QTY. PERFORMED ALTERNATE GEAR EXTENSION. FOUND PYLON PRESSURE LINE CHAFING AND WORN THROUGH. CUT, REMOVED AND INSTALLED NEW LINE. LEAK CHECKS OK.
F/A REPORTED ODOR AND HAZE IN CABIN JUST PRIOR TO DESCENT. LATER REPORTED HAZE AND MOST OF SMELL HAD CLEARED. TROUBLESHOT. NO TROUBLE FOUND. PERFORMED DUCT BURNOUT AND REPLACED COALESCER BAGS.
EMERGENCY LIGHT INOPERATIVE VENTRAL STAIR AREA. REPAIRED IAW SWPM. OPS CHECKED GOOD.
FUSELAGE OUTER SKIN DAMAGE AT THE L1 DOOR GUST LOCK PIN CUTOUT. PERFORMED DVI. NO OTHER DAMAGE NOTED. TRIMMED OUT DAMAGED SKIN IAW RI 524991-14. COMPLETED IAW REPAIR INSTRUCTIONS 524991-14.
DURING SERVICE CHECK, EMERGENCY EXIT LIGHTS IN CEILING AT ROWS 24 AND 25 INOPERATIVE. FOUND BATTERY PACK NOT CONNECTED. RECONNECTED AT LOCATION B5-243. OPS CHECKS GOOD.
AFT ACCESSORY BAY AREA, CRACK AROUND FASTENER AREA BS 1520, LBL 10. ROUTED OUT CRACKED AREA AND FABRICATED REPAIR DOUBLER & SHIMS IAW ER/A 504832-14.
DURING HMV, CORROSION WAS FOUND ON THE RT WING CENTER SECTION UPPER WING SKIN AT STA 954 AND BL 0. SUBSEQUENTLY, THE CORROSION WAS R & R IAW ER/A 504829-14. ACCOMPLISHED SECTION 1 OF REPAIR IAW ER/A 504829-14, REV O. REMOVED CORROSION FROM CENTER TANK, RBL 58, BS 955 IAW SRM 51-10-03, PARA 26 VOL II UT AREA AND FOUND TO BE OUT OF LIMITS IAW NDT SPM, PART 4 04-00-07, & SRM 53-00-01, FIG 3, VOL I. ORIG .235 AND LOWEST DEPTH IS .112 HFEC AREA IAW NDTSPM PART 6, 06-10-01 AND FOUND NO ADDITIONAL DEFECT OR CRACKS. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW ER/A 504829-14, REV 14, SEC 1 CAPPED SEAL ALL TANK FASTENERS IAW SRM 51-20-00, PARA 9, VOL II.
L1 DOOR INTERIOR BEAM CRACKED IN RADIUS AFT SIDE VIEWED THROUGH LIGHTNING HOLE STA 198. STOP DRILLED CRACK .250 DIA, LOCATED AND DRILLED NEW ANGLE AND INSTALLED IAW ERA 504823-14 REV 0, DWG 9955752 AND SRM 51-40-01, 51-40-02 AND 51-40-05. ASSOCIATED ER/A 14-504823 ADDED FOR AC 9238.
FORWARD ENTRY DOOR INTERNAL UPPER BEAM CRACKED IN RADIUS SIDE VIEWED THROUGH LIGHTNING HOLE STA 167. STOP DRILLED CRACK .250 DIAMETER IAW ERA 504823-14 AND SRM 51-00-01. LOCATED AND DRILLED NEW ANGLE IAW ERA 504823-14, REV 0 AND DWG 9955752. INSTALLED REPAIR ANGLE IAW SRM 51-40-01 AND 51-40-05. ASSOCIATED ER/A 14-504823 ADDED FOR AC 9238.
FUSELAGE LONGERON FITTING CRACKED. REPAIRED AT BS 1060, L20R IAW ER/A 14-509933 ADDED FOR AC 9238.
DURING CHECK, FOUND LT WINGTIP L/E HORN GOUGED, WS 560. FOUND HORN OUT OF LIMITS. REMOVED HORN FROM L/E. WELDED, GROUND WELD FLUSH, HFEC AND MT. NO DAMAGE NOTED. ALODINED, PRIMED AND INSTALLED HORN ON LEFT WINGTIP L/E SRM 51-30-02, 51-10-03 AND ER/A 468102-14 MA, ADDED FOR AC 9238. ACFT OK FOR SERVICE.
AFT AIRSTAIR (3RD STAIR FROM THE TOP, ABOVE THE APU ENCLOSURE) AFT RT CORNER HAS EVIDENCE OF CORROSION. R & R LOWER TEE ANGLE IAW SRM 51-10-05, 51-30-02, 51-30-05, 51-10-03 AND AMM 51-10-00-370-802.
CORROSION AT AFT CARGO BS 1379 FRAME. AFT SIDE AT L30. REMOVED CORROSION. AREA FOUND OUT OF LIMITS WITH 100 PERCENT MATERIAL LOSS. CUT OUT DAMAGED AREA. FABRICATED TWO REPAIR SPLICES AND NEW FORMER. REPAIR INSTALLED IAW SRM 53-00-01, FIG 1 AND 51-10-03 PARA 26, PARA 21, PARA 1, VOL II AND 53-10-02, FIG 3, VOL I.