N836US
Registered owner: USA JET AIRLINES INC, MI (owner ≠ operator)
Operators of this aircraft
Who operated this tail, and how firmly we know it.
No operator established for this aircraft.
Accident & incident history
No NTSB accidents or incidents on file for this aircraft.
Maintenance disclosures
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND CORROSION ON A CUSP WEB ANGLE AT F.S. 218 LBL 54 IN THE DOOR JAMB AREA. CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND THE CORROSION TO BE OUT OF LIMITS. THEY TRIMMED OUT DAMAGED SECTION OF THE DOOR JAMB. THEY PERFORM A HFEC INSPECTION OF THE TRIMMED SECTION OF THE REPAIR, NO CRACK INDICATIONS OR ANY OTHER DAMAGE INDICATIONS NOTED. THEY FABRICATED A EO18667-11 CUSP ANGLE FROM .063â 7075-T6, A EO18667-13 FILLER FROM .040â 7075-T6 AND A EO18667-15 TAPERED SHIM FROM 7075-T6. ALL REPAIR PARTS WERE DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-03. ALL REPAIR PARTS WERE INSTALLED AT F.S. 218 LBL IAW FIG. 3 OF EO18667 IR. REPAIR WAS APPROVED BY 8110-3 DATED 8/17/22 BY RICARDO FERNANDEZ DERT-834363-CE
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND CORROSION ON THE CUSP WEB AND FLOOR WEB AT F.S. 215 RBL 58 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND IT TO BE OUT OF LIMITS. THEY TRIMMED OUT DAMAGED SECTION OF THE CUSP ANGLE IAW EO18305 FIGURE 2. THEY FABRICATED A EO18305-11 CUSP ANGLE FROM .071â 7075-T6, A EO18305 -13 UPPER DOUBLER ANGLE FROM .080â 7075-T6, A EO18305-15 LOWER FILLER FROM .090â 7075-T6, A EO18305-17 LOWER DOUBLER FROM .080â 7075-T6 AND EO18305-19 FILLER FROM .071â 7075-T6 IAW FIG 3 OF EO18305. ALL REPAIR PARTS WERE DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9/MD80 SRM 51-20-03. ALL REPAIR PARTS WERE INSTALLED WET IAW FIG. 3 OF EO18305. REPAIR APPROVED BY 8110-3 DATED 8/4/2022 BY RICARDO FERNANDEZ DERT-834363-CE
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND AREAS OF CORROSION ON THE MAIN CABIN SEAT TRACK BETWEEN F.S. 200 -275 RBL 54.5 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE SEAT TRACK AND FOUND IT TO BE OUT OF LIMITS. THEY REMOVED THE CORRODED SEAT TRACK BETWEEN F.S. 200-275 RBL 54.5 IAW DC9/MD80 SRM 53-05. THEY FABRICATED, DRILLED AND DEBURRED THE SEAT TRACK FROM S00482-7075T76511 AND REPAIR SPLICE PARTS FROM 3925837-501, .063â 7075-T6 AND .100â 7075-T6.REPAIR PARTS WERE TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-3.THEY INSTALLED THE SEAT TRACK AND REPAIR PARTS BETWEEN F.S. 200-275 RBL 54.5 IAW DC9/MD80 SRM 53-05
DISCREPANCY: WHILE AT C-CHECK IN KDHN, COMMERCIAL JET FOUND A FRAME CORRODED AT F.S. 1322 AND LONGERON 30 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN FOUND THE FRAME AT F.S. TO BE CORRODED OUT OF LIMITS. THEY CUT OUT DAMAGED SECTION OF THE FRAME AT F.S. 1322BETWEEN LONGERONS 27L AND 27R IAW DC9/MD80 SRM 53-03 FIG. 2A. THEY FABRICATED NEW FRAME FROM .063â 7075-0 AND ALSO FABRICATED 4 EACH SPLICES FROM .071â 7075-0 IAW DC9/MD80 SRM 53-03 FIG. 2A..REPAIR PARTS WERE HEAT TREATED FROM 0 TO T6 CONDITION. THEY FABRICATED FORWARD AND AFT PLATE REPAIR PIECES FROM .063â 7075-T6. IAW DC9/MD80 SRM 53-03 FIG. 2A. THEY LOCATED, DRILLED AND DEBURRED, TREATED AND PRIMED THE FRAME, FRAME SPLICES AND FORWARD AND AFT PLATE REPAIR. THEY INSTALLED REPAIR PARTS (FRAME, FRAME SPLICES AND FWD. AND AFT PLATES REPAIR) IAW DC9/MD80 SRM 53-033 FIG. 2A
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND LONGERON 25L CORRODED AT STATION 1287 IN THE AFT LOWER CARGO COMPARTMENT CORRECTIVE ACTION: CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND THE CORRODED AREA OUT OF LIMITS IAW DC9/MD80 SRM 51-30-5. THEY REMOVED THE SECTION OF LONGERON 25L BETWEEN F.S. 1280 AND 1300.THEY CUT, DRILLED AND DEBURRED LONGERON SECTION FROM 2912727-7075T6511 AND CUT, DRILLED AND DEBURRED REPAIR SPLICE FITTINGS FROM 3913291U501. TREATED AND PRIMED LONGERON SECTION AND SLICE FITTING PARTS IAWDC9/MD80 SRM 51-10-3. THEY INSTALLED LONGERONS AND SPLICES IN THE AFT CARGO COMPARTMENT BETWEEN F.S. 1280 AND 1300 IAW DC9/MD80 SRM 51-30-5 AND SRM 51-30-2
DISCREPANCY: DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND LONGERON 24L CORRODED BETWEEN STATIONS 1287 AND 1309 IN THE AFT LOWER CARGO COMPARTMENT CORRECTIVE ACTION: CORRECTIVE ACTION: CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND THE CORRODED AREA OUT OF LIMITS IAW DC9/MD80 SRM 51-30-5. THEY REMOVED THE SECTION OF LONGERON 24L BETWEEN F.S. 1280 AND 1300.THEY CUT, DRILLED AND DEBURRED LONGERON SECTION FROM 2912727-7075T6511 AND CUT, DRILLED AND DEBURRED REPAIR SPLICE FITTINGS FROM 3913291U501. TREATED AND PRIMED LONGERON SECTION AND SLICE FITTING PARTS IAWDC9/MD80 SRM 51-10-3. THEY INSTALLED LONGERONS AND SPLICES IN THE AFT CARGO COMPARTMENT BETWEEN F.S. 1280 AND 1300 IAW DC9/MD80 SRM 51-30-5 AND SRM 51-30-2
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND A MAIN CABIN FLOOR BEAM CORRODED ON THE UPPER AND LOWER SURFACE AT F.S. 1322, LBL54 TO RBL54 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE FLOOR BEAM AND FOUND THE CORROSION TO BE OUT OF LIMITS. THEY TRIMMED OUT SECTION OF FLOOR BEAM IAW EO18214. PERFORMED HFEC OF THE TRIMMED-OUT AREA AND FOUND NO CRACK INDICATIONS. THEY FABRICATED A REINFORCEMENT ANGLE P/N EO18214-11 FROM .100â 7075-T6, A FILLER P/N EO18214-13 FROM.100â 7075-T6 AND A STRAP P/N EO18214-15 FROM >100â 7075-T6. ALL REPAIR PARTS WERE DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-03. REPAIR PARTS WERE INSTALLED IAW EO18214. REPAIR 8110-3 APPROVED BY RICARDO FERNANDEZ DERT-834363-CE
DISCREPANCY: DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND A MAIN CABIN FLOOR BEAM CORRODED ON THE UPPER AND LOWER SURFACE AT F.S. 1338, LBL54 TO RBL54 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE FLOOR BEAM AND FOUND THE CORROSION TO BE OUT OF LIMITS. THEY TRIMMED OUT SECTION OF FLOOR BEAM IAW EO18212. PERFORMED HFEC OF THE TRIMMED-OUT AREA AND FOUND NO CRACK INDICATIONS. THEY FABRICATED A REPAIR FILLER P/N EO18212-11 FROM .100â 7075-T6, A REPAIR STRAP P/N EO18212-13 FROM.100â 7075-T6 IAW EO18212. ALL REPAIR PARTS WERE DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-03. REPAIR PARTS WERE INSTALLED IAW EO18212. REPAIR 8110-3 APPROVED BY RICARDO FERNANDEZ DERT-834363-CE
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND THE FUSELAGE FRAME AT F.S. 110 LH CRACKED BELOW FLIGHT DECK WINDOW CORRECTIVE ACTION: COMMERCIAL JET IN KDHN VERIFIED CRACKED FRAME. THEY CUTOUT CRACKED SECTION OF FRAME SECTION IAW DC9/MD80 SRM 51-70-5. THEY FORMED FRAME REPAIR SECTION FROM .063â 7075-0 AND REPAIR DOUBLER FROM .071â 7075-0 IAW DC9/MD80 SRM 51-10-2 AND 51-70-5. HEAT TREATED REPAIR PARTS FROM 0 TO T6. THEY DRILLED, DEBURRED, AND TREATED AND PRIMED FORMED FRAME REPAIR SECTION AND REPAIR DOUBLER IAW DC9/MD 80 SRM 51-10-3. THEY INSTALLED FRAME REPAIR SECTION AND REPAIR DOUBLER ON FRAME AT STATION 110 LH BELOW FLIGHT DECK WINDOW IAW DC9/MD80 SRM 51-70-5 FIG. 1 AND SRM 51-30-5
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND HOLE DAMAGE ON L8L UPPER INBOARD FLANGE BETWEEN FRAMES 1401 AND 1418 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN, INSPECTED DAMAGE AND FOUND TO BE OUT OF LIMITS. THEY CUTOUT DAMAGE SECTION OF L8L BETWEEN F.S. 1392 AND 1428. THEY FABRICATED, DRILLED AND DEBURRED NEW SECTION OF L8L FROM 2777922-3-7075-T6. THEY ALSO FABRICATED DRILLED AND DEBURRED SPLICE REPAIR FROM 7637813-3-7075-T6. ALL REPAIR PARTS WERE TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-3. THEY INSTALLED NEW LONGERON SECTION AND LONGERON REPAIR SPLICES ON L8L BETWEEN STATIONS 1392 AND 1428 IAW DC9/MD80 SRM 53-14-4 AND SRM 53-02 FIG.18
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND LONGERON 22L CORRODED BETWEEN STATIONS 1271 AND 1338 IN THE AFT LOWER CARGO COMPARTMENT CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND THE CORRODED AREAS OUT OF LIMITS IAW DC9/MD80 SRM 51-30-5. THEY REMOVED 3 SECTIONS OF LONGERON 22L BETWEEN F.S. 1271-1338.THEY CUT, DRILLED AND DEBURRED LONGERON SECTIONS FROM 5242886-7075T6511 AND CUT, DRILLED AND DEBURRED REPAIR SPLICES FROM 52642454-7075T6 SPLICE EXTRUSION. TREATED AND PRIMED LONGERON SECTIONS AND SLICE REPAIR PARTS IAWDC9/MD80 SRM 51-10-3. THEY INSTALLED LONGERONS AND SPLICES IN THE AFT CARGO COMPARTMENT BETWEEN F.S. 1271 AND 1338 IAW DC9/MD80 SRM 51-30-5 AND SRM 51-30-2
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL FOUND AREAS OF CORROSION ON THE SEAT TRACK IN THE MAIN CABIN BETWEEN F.S. 218 AND 788 LBL 54.00 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREAS AND FOUND THEM TO OUT OF LIMITS. THEY REMOVED DAMAGED SEAT TRACK FROM F.S. 218 TO 370 AND F.S. 560 TO 797 IAW DC9/MD80 SRM 53-40-00. THEY FABRICATED, DRILLED AND DEBURRED SEAT TRACK SECTIONS FROM F.S. 218-370 AND F.S. 560-797 FROM S00482-7075T76511 AND FABRICATED, DRILLED AND DEBURRED 5 EACH SPLICES FROM .125â 7075-T6. TREATED AND PRIMED ALL REPAIR PARTS IAW DC9/MD80 SRM 51-10-3. THEY INSTALLED 2 EACH SEAT TRACKS AND 5 EACH SPLICES BETWEEN F.S.218 AND 370 AND F.S. 560-797 IAW DC9/MD80 SRM 53-05 AND SRM 51-10-3
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND NUMEROUS AREAS OF CORROSION ON THE MAIN CABIN SEAT TRACK BETWEEN STATIONS 275 AND 797 RBL 54.5 CORRECTIVE ACTION: COMMERCIAL JET IN KDHN INSPECTED THE AREA AND FOUND THE AREA FROM F.S. 537-788 TO BE OUT OF LIMITS. THEY REMOVED CORROSION FROM SEAT TRACK BETWEEN STATIONS 275-537(.015â) AND 789â797 (.010â), ORIGINAL THICKNESS .080â,THESE AREAS FOUND TO BE WITHIN LIMITS, AREAS WERE TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-3. THEY REMOVED THE DAMAGED SEAT TRACK BETWEEN STATIONS 537-788 IAW DC9/MD80 SRM 53-05 FIG.4F.THEY FABRICATED, DRILLED AND DEBURRED SEAT TRACK FROM S00482-7075T76511 AND REPAIR SPLICES FROM.063â 7075-T6 AND .100â 7075-T6. ALL REPAIR PARTS WERE TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-3. THEY INSTALLED SEAT TRACK AND REPAIR PARTS BETWEEN F.S. 537 AND 788 RBL 54.5 IAW DC9/MD80 SRM 53-05 FIG. 4F
DISCREPANCY: DURING C-CHECK IN KDHN, COMMERCIAL JET FOUND A PLUGGED HOLE AT STATION 315 L16L CORRECTIVE ACTION: COMMERCIAL JET IN KDHN PERFORMED A HFEC INSPECTION OF THE AREA AND FOUND THE HOLE TO BE CRACKED. THEY TRIMMED OUT THE DAMAGE AREA IAW FIG 3 OF EO17365. THEY PERFORMED A HFEC INSPECTION OF THE TRIMMED-OUT AREA AND FOUND NO CRACK INDICATIONS OR OTHER DAMAGE. THEY FABRICATED 2 EACH EO17365-11 DOUBLERS FROM .050â 2024-T3, 2 EO17365-13 FILLERS FROM .050â 2024-T3, A EO17365-15 FREEZE PLUG FROM .050â 7075-T6 AS SHOWN IN FIG 2 AND STEP 13 OF EO17365 AND EO17365-17 FILLER FROM .050â 7075-T6. ALL REPAIR PARTS WERE DRILLED, DEBURRED, TREATED AND PRIMED IAW DC9/MD80 SRM 51-10-03.REPAIR PARTS WERE INSTALLED IAW FIG 2 OF EO17365. REPAIR APPROVED BY 8110-3 DATED 6/12/0222 BY RICARDO FERNANDEZ DERT-834363-CE