N834US
Registered owner: USA JET AIRLINES INC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
| Operator | Role | Period | Basis |
|---|---|---|---|
| USA JET AIRLINES, INC. (Y2PA) | Operator | 2023-03-24 – 2023-03-24 | Operator named in NTSB report |
Accident & incident history
Maintenance disclosures
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND A DRAG MARK ON THE FUSELAGE SKIN AT APPROXIMATELY F.S. 1322 L30, AND THE SKIN GOUGED BETWEEN F.S. 1334 TO 1338, L29L â L29R. MAINTENANCE IN KYIP PERFORMED A HFEC INSPECTION OF THE DAMAGE AREA AND VERIFIED NO CRACKS AND NOM THICKNESS OF 0.061â AND MIN THICKNESS OF 0.044â IN THE DAMAGED AREA. C.A.S MAINTENANCE FABRICATED A REPAIR DOUBLER FROM DMS 1592 0.025â MATERIAL, DOUBLER WAS TREATED, PRIMED AND INSTALLED IAW DC9/MD80 SRM 53-04-1 PARA. C PAGE 8 AND DRAWING # 5911429
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND A SKIN PANEL IS GROUND DOWN AT F.S. 1381, L23R-L28R. . MAINTENANCE IN KYIP REMOVED AND CUT OUT DAMAGE. USA JET MAINTENANCE PERFORMED A HFEC INSPECTION OF THE AREA AND VERIFIED NO CRACKS PRESENT. CAS FABRICATED A FILLER AND A DOUBLER FROM TITANIUM 0.025â REPAIR PARTS WERE TREATED, PRIMED AND INSTALLED IAW SRM 53-04, SHEET 4
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND A CRACK ON THE R/H OUTER FRAME, OUTER FRAME CAP AT F.S. 1380, L22R-L23R. MAINTENANCE IN KYIP REMOVED AND CUT OUT DAMAGE. USA JET MAINTENANCE PERFORMED A HFEC INSPECTION OF THE AREA AND VERIFIED ALL DAMAGE WAS REMOVED. CAS FABRICATED 2 EA. REPAIR ANGLES FROM 7075-T6 0.063â, 1 EA. FILLER FROM 7075-T6 0.090â AND 2 EA. REPAIR STRAPS FROM 7075-T6 0.063â.ALL REPAIR PARTS WERE TREATED , PRIMED AND INSTALLED IAW TD # 0079-CAS-201 IR AND FAA FORM 8110-3 DATED 7/26/2023.
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND THE SKIN GROUND DOWN AND DENTED BETWEEN L29L-L29R AT F.S. 1338-1363. MAINTENANCE IN KYIP PERFORMED CUTOUT OF DAMAGED AREA, MAINTENANCE PERFORMED A HFEC INSPECTION OF THE AREA AND VERIFIED NO FURTHER DAMAGE EXISTED. C.A.S. MAINTENANCE FABRICATED A REPAIR SKIN FROM A NEW SKIN P/N 5911429-151. REPAIR SKIN SECTION WAS TREATED, PRIMED AND INSTALLED IAW DC9/MD80 SRM 53-01, PARA. 2B
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND THE AFT PRESSURE BULKHEAD TEE SEVERED AND BENT BETWEEN F.S. 1334-1338 AT BL 0. . MAINTENANCE IN KYIP REMOVED THE DAMAGED APB TEE AND INSTALLED A NEW TEE IAW SRM 53-03, FIGURE 33.
DURING A TAIL-STRIKE INSPECTION IN KYIP, MAINTENANCE FOUND THE SKIN IS GROUND OFF BETWEEN F.S. 1331-1338, BETWEEN L29L AND L29R. MAINTENANCE IN KYIP REMOVED AND CUT OUT DAMAGED SKIN BETWEEN F.S. 1331-1338, L29L- L29R, MAINTENANCE PERFORMED A HFEC INSPECTION OF THE AREA AND VERIFIED ALL DAMAGE WAS REMOVED. FABRICATED A INTERNAL DOUBLER FROM 2024 T3 0.025â, FILLERS FROM 2024 T3 0.063 AND AN EXTERNAL DOUBLER FROM 7075 T6 0.071â. THEY TREATED, PRIMED AND INSTALLED REPAIR PARTS IAW SRM 53-04 PARA. 8, FIGURE 9
DURING A TAIL-STRIKE INSPECTION IN KYIP, C.A.S. MAINTENANCE FOUND THE APB WEB DENTED AND CRACKED, L=20â W=58â DEPTH=0.050â AT F.S 1334-1338. MAINTENANCE IN KYIP PERFORMED THE DAMAGE CUTOUT OF THE APB SKIN, MAINTENANCE PERFORMED A HFEC INSPECTION AND VERIFIED ALL DAMAGE WAS REMOVED. FABRICATED A NEW REPAIR SKIN FROM P/N 5910130-285, REPAIR Y-CHORD FROM P/N 5910130-387, REPAIR SPLICE -5 FROM 2024-T3, REPAIR SPLICE -7 FROM 2024-T3 0.063â, REPAIR PLATE -13 FROM 2024-T3 0.063âAND REPAIR DOUBLER -11 FROM 7075-T6 0.080â. ALL REPAIR PARTS WERE TREATED, PRIMED AND INSTALLED IAW SRM 53-03 PARA. 7 FIG. 33-PAGE 2B AND 53-03 FIGURE 37.