# N571UA: Zipline International P2 ZIP

- Status: Valid registration
- Airframe: [Zipline International P2 ZIP](https://openairdocs.org/model/zipline-international-p2-zip) (registry code 06102II)
- Serial number: 18736P22251
- Type: Hybrid lift
- Engine type: Electric
- Certificate issued: May 6, 2026
- Expires: May 31, 2033
- Mode S code: A753E3
- Registered owner: [Zipline International Inc](https://openairdocs.org/faa-owner/ZIPLINE%20INTERNATIONAL%20INC)
- Location: [S San Fran, CA](https://openairdocs.org/faa-place/CA/S%20San%20Fran)
- Owner type: Corporation
- Owner's area on the map: 37.6552° N, 122.4184° W: Placed by OpenAirDocs at the center of ZIP code 94080, within about 2 miles (OpenAirDocs). The owner's mailing address, not where the aircraft is based
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=571UA
- Page: https://openairdocs.org/aircraft/N571UA

From the FAA registry file of October 24, 2026. ADs below are matched by the registry's airframe and engine model codes. They may apply; each AD's applicability can narrow it by serial number, part number or installed equipment. This is not a compliance determination.

## ADs that may apply (OpenAirDocs): 0 in force

### Matched by airframe (Zipline International P2 ZIP)

None in force.

## Information bulletins (advisory)

None matched.

## NTSB investigations

None matched to N571UA.

## NTSB investigations on N571UA not matched to an aircraft (1)

From the NTSB's public API. Aircraft are matched to registry aircraft by N-number and event date, checked against the reported serial number, make and model; the registry's history has gaps, so older matches can be wrong. Compare the reported make and model.

- [NTSB DCA11CA073](https://openairdocs.org/ntsb/DCA11CA073), Jun 12, 2011: Boeing 757-222 (N571UA), San Fransico, CA, substantial damage. Probable cause: The ramp personnel's failure to visually verify the position of the jetway before beginning the airplane pushback.

## FAA accident and incident reports

None matched to N571UA.

## Service difficulty reports

None filed for this aircraft. Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

## Service difficulty reports on N571UA not matched to an aircraft (121, newest 50)

They name N571UA, but no registry record covers the date, the aircraft registered then was built later, or the report describes another aircraft.

- [SDR FDEA201408272331](https://openairdocs.org/sdr/FDEA201408272331), Aug 27, 2014: REPAIR. CORRODED. STATION 1640 FLOORBEAM HAS CORROSION ON REPAIR RBL 47. REMOVED CORROSION & FOUND OUT OF LIMITS BY EXFOLIATION IAW SRM 53-00-51 DETAIL III. REMOVED FLOORBEAM IAW
- [SDR FDEA201408252308](https://openairdocs.org/sdr/FDEA201408252308), Aug 25, 2014: STRINGER. CORRODED. AFT CARGO PIT STATION 1616 CORROSION ON STRINGER AT SPLICE. EVALUATED CORROSION ON AFT CARGO STATION 1616 STRINGER 19R AT SPLICE. NO ALLOWED DAMAGED ON SRM. REP
- [SDR FDEA201408072112](https://openairdocs.org/sdr/FDEA201408072112), Aug 7, 2014: SEAT TRACK. GOUGED. SEAT TRACK, BS 440-650 LBL 45 NICKED AND GOUGED FOUND TO BE OUT OF LIMITS IAW SRM 53-00-52 FIG 101 DETAIL XI PAGE 106. FABRICATED NEW SEAT TRACK IAW SRM 53-30-5
- [SDR FDEA201408052073](https://openairdocs.org/sdr/FDEA201408052073), Aug 5, 2014: SEAT TRACK. DAMAGED. MAIN CABIN BTW BS900 BS1080 LBL 24.75 SEAT TRACK HAS GOUGES, NICKS AND CORROSION IN SEVERAL PLACES REMOVED AND REPLACED SEAT TRACK CROWN MATERIAL BAC1520-792A B
- [SDR FDEA201407251977](https://openairdocs.org/sdr/FDEA201407251977), Jul 25, 2014: PRESSURE DECK. CORRODED. PRESSURE DECK AT BS 1681 - 1720, RBL 62 - LBL 62 SEVERAL SPOTS FOUND CORRODED. REPAIRED IAW EA F-5310-T0312899. MAJOR REPAIR.
- [SDR CALA2013102492356](https://openairdocs.org/sdr/CALA2013102492356), Oct 23, 2013: GIRT BAR. STUCK. DOOR 4R WON'T ARM. UNSTUCK GIRT BAR & CYCLED 4R ARM DISARM HANDLE SEVERAL TIMES. NO TROUBLE NOTED, INDICATION NORMAL.
- [SDR CALA2013100991886](https://openairdocs.org/sdr/CALA2013100991886), Oct 8, 2013: PLUG. LOOSE. HYD FLUID LEAKING FROM LT WING OTBD SPOILER ACTUATOR. FOUND UPPER PLUG ON ACTUATOR LOOSE. SECURED & LEAK CHECKED. NO LEAKS NOTED.
- [SDR CALA2013080790224](https://openairdocs.org/sdr/CALA2013080790224), Aug 6, 2013: SKIN. DELAMINATED. RIGHT WING T/E BETWEEN INBD AND OTBD FLAP HAS AREA OF DELAMINATION. REMOVED DAMAGE REPAIR REF SRM 51-70-10, REF ALSO SRM 57-53-01.
- [SDR UALA2013062704490](https://openairdocs.org/sdr/UALA2013062704490), Jun 26, 2013: CONTROL PANEL. DAMAGED. FLIGHT DECK WET WITH HIGH HUMIDITY. REPLACED VHF COMM 1 & 2 CONTROL PANELS IAW AMM. REPLACED ADF CONTROL PANEL IAW AMM. REPLACED RT EFIS CONTROL PANEL IAW AMM. 
- [SDR UALA2013061704169](https://openairdocs.org/sdr/UALA2013061704169), Jun 15, 2013: FRAME. GOUGED. A GOUGE AT STA 1640, ABOVE STR 9L. REPAIRED GOUGE AT BS1640 FRAME UPPER FLANGE APPROX 1.25" ABOVE STR 9L.
- [SDR UALA2013061704167](https://openairdocs.org/sdr/UALA2013061704167), Jun 15, 2013: SKIN. DENTED. DENT ON FUSELAGE SKIN AT BS 270 STR 21-22R. REPAIRED DENT AT FUSELAGE SKIN AT 270 STR 21R-22R IAW SRM 53-00-01, FIG 201, REPAIR 3.
- [SDR UALA2013061304055](https://openairdocs.org/sdr/UALA2013061304055), Jun 12, 2013: SKIN. DENTED. RT APU DOOR FWD EDGE MEMBER HAS A DENT 24 INCHES AFT OF FWD EDGE. REPAIRED RT APU DOOR FWD EDGE IAW SRM 51-70-11. NDT INSPECTED CUTOUT IAW NTM 51-00-19 AND 16 N
- [SDR CALA2013082790799](https://openairdocs.org/sdr/CALA2013082790799), Jun 10, 2013: SKIN. DENTED. IAW CF9083 & CF9084. DENTS AT BS 1490 & 1495 BETWEEN STRINGER 22L & 23L. CUTOUT & REPAIRED DENTS AT BS 1490 & 1495 AT STRINGER 22L - 23L IAW SRM 53-00-01 FIG 20
- [SDR UALA2013061204016](https://openairdocs.org/sdr/UALA2013061204016), Jun 9, 2013: SKIN. DENTED. DENT ON LOWER EXTERIOR FUSELAGE SKIN JUST FWD OF REPAIR DOUBLER AT BS 1601, S30R. REPAIRED DAMAGE ON LOWER EXTERIOR FUSELAGE SKIN AT BS 1595-1615 S29-30R IAW SR
- [SDR UALA2013061103994](https://openairdocs.org/sdr/UALA2013061103994), Jun 8, 2013: SKIN. DENTED. ON WALK AROUND, FOUND A DENT AT BS 1495 BETWEEN S22-23L. DENT MEASURES 2.5" WIDE, 3.5" LONG AND 3-32 (.09375) DEEP. CUTOUT AND REPAIRED SKIN.
- [SDR UALA2013060603912](https://openairdocs.org/sdr/UALA2013060603912), Jun 5, 2013: SKIN. DENTED. FUSELAGE SKIN HAS PROTRUDING DENT BS 520 STR 24L. REPAIRED DENT IN FUSELAGE SKIN AT BS 520, STR 24L IAW SRM 53-00-01, FIG 201, REPAIR 2. MAJOR REPAIR.
- [SDR UALA2013060403863](https://openairdocs.org/sdr/UALA2013060403863), Jun 3, 2013: SKIN. DAMAGED. EXTERNAL SKIN HAS A LIGHTNING STRIKE AT BS 552 FIVE INCHES BELOW S28R. REPAIRED SKIN IAW SRM 53-30-01, FIG 1 AND SRM 53-00-01, FIG 101. NDT INSPECTION IAW NTM P
- [SDR UALA2013060303826](https://openairdocs.org/sdr/UALA2013060303826), May 31, 2013: SKIN. DAMAGED. EXTERNAL SKIN HAS INDICATION OF LIGHTNING STRIKES AT BS 480, STR 25R. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.
- [SDR UALA2013053103812](https://openairdocs.org/sdr/UALA2013053103812), May 30, 2013: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 211 EIGHT INCHES LEFT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.
- [SDR UALA2013053103804](https://openairdocs.org/sdr/UALA2013053103804), May 30, 2013: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 208, 8.5" LEFT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 2, 01.
- [SDR UALA2013053103803](https://openairdocs.org/sdr/UALA2013053103803), May 30, 2013: SKIN. DAMAGED. LIGHTNING STRIKE AT BS 220 7.5" LT OF BL 0. REPAIRED SKIN IAW SRM 53-00-01, FIG 201.
- [SDR UALA2013042402841](https://openairdocs.org/sdr/UALA2013042402841), Apr 24, 2013: LIGHT. INOPERATIVE. EMERGENCY LIGHT OUTSIDE OF MID LAVATORY INOPERATIVE. REPLACED EMERGENCY LIGHT ASSY.
- [SDR UALA2013042402855](https://openairdocs.org/sdr/UALA2013042402855), Apr 23, 2013: LIGHT. INOPERATIVE. EEL OUTSIDE OF MID LAV INOP. MID LAV EEL STRIP INOPERATIVE.
- [SDR UALA2013040202154](https://openairdocs.org/sdr/UALA2013040202154), Apr 1, 2013: FLOOR PANEL. DELAMINATED. SOFT SPOT II AISLE FLOOR ROW 39. FOUND DELAM AREA MEASURED 22" ACROSS. PERFORMED INTERIM REPAIR REF AMM 53-00-99 PG 801. OVERLAY TAPED AND FASTENER HOLES PICKED
- [SDR UALA2013040102083](https://openairdocs.org/sdr/UALA2013040102083), Apr 1, 2013: SHUTOFF VALVE. FAULTY. ENGINE DUCT PRESSURES SPLIT DURING TAKEOFF OR CLIMB. REPLACED NR 1 ENGINE PRSOV IAW AMM & REPLACED NR 1 ENG PRSOV REGULATOR IAW AMM.
- [SDR UALA2013010700105](https://openairdocs.org/sdr/UALA2013010700105), Jan 5, 2013: SMOKE DETECTOR. NOISY. L1 DOOR SQUEAL IS EXTREMELY LOUD AND UNBEARABLE FOR FLIGHT ATTENDANTS. DURING PRESSURIZATION FOR TROUBLESHOOTING, SQUEAL COMING FROM THE FWD LAV. REMOVED AND RE
- [SDR UALA2012122107363](https://openairdocs.org/sdr/UALA2012122107363), Dec 20, 2012: BOTTLE. LOW PRESSURE. AFT O2 BOTTLE WAS USED PRESSURE IS LOW. PRESSURE IS LOW. REMOVED BOTTLE AND INSTALLED STICKER TO BRACKET.
- [SDR UALA2012110506343](https://openairdocs.org/sdr/UALA2012110506343), Nov 5, 2012: PIN. BROKEN. EMERGENCY LIGHT STRIP ON FLOOR AT C12 LOOSE WIRES. FWD OF ROW 12 EMER FLOOR STRIP INOP. CONNECTOR PIN BROKEN. REMOVED AND SOLDERED POWER STRIP AS PER INTERIM RE
- [SDR UALA2012101805968](https://openairdocs.org/sdr/UALA2012101805968), Oct 17, 2012: O-RING. LEAKING. FUEL LEAK RIGHT WING, IN THE MLG FWD TRUNNION AREA. REPLACED O-RINGS ON SHUT-OFF VALVE ACTUATOR, REF MM 28-21-1.
- [SDR UALA2012101805967](https://openairdocs.org/sdr/UALA2012101805967), Oct 16, 2012: CONTROL VALVE. FAULTY. RIGHT WING SHUTOFF VALVE WILL NOT OPEN. COMPLIED WITH MEL. REPLACED RIGHT WING CONTROL VALVE IAW AMM.
- [SDR UALA2012101505876](https://openairdocs.org/sdr/UALA2012101505876), Oct 13, 2012: ACTUATOR. LEAKING. HYD FLUID LEAKING FROM RIGHT OUTBOARD WING UNDER NUMBER 12 SPOILER AREA. REMOVED NR 12 SPOILER ACTUATOR. MEASUREMENT FROM BOTTOM OF LOCKNUT TO PCA ROD IS .326 R
- [SDR UALA2012080604177](https://openairdocs.org/sdr/UALA2012080604177), Aug 5, 2012: LIGHT. INOPERATIVE. FOUND AFT EMEGENCY LIGHT NOT WORKING. REPLACED EMERGENCY LIGHT.
- [SDR UALA2012070903656](https://openairdocs.org/sdr/UALA2012070903656), Jul 6, 2012: GUARD. FAULTY. EMERGENCY LIGHTS SWITCH COVER DOES NOT ARM SWITCH WHEN CLOSED. REPLACED P5 PANEL EMERGENCY LIGHT SWITCH GUARD.
- [SDR UALA2012052102858](https://openairdocs.org/sdr/UALA2012052102858), May 20, 2012: FILTER. FAULTED. LEFT ENGINE OIL FILTER EICAS AND STATUS MESSAGE AFTER ENGINE START, OIL TEMP 69C. RETURNED TO BLOCKS, REPLACED MAIN OIL FILTER AND PER MM 79-21-05 P 401, AND OI
- [SDR UALA2012051602784](https://openairdocs.org/sdr/UALA2012051602784), May 13, 2012: OIL SYSTEM. OVERSERVICED. NR 1 ENG HIGH OIL CONSUMPTION EXCEEDS LIMIT, CHECKED OVER ENGINE AND COULD FIND NO EVIDENCE OF ANY LEAKS. REVIEW OF OIL SERVICE HISTORY AND SUSPECT THE PREVIOUS
- [SDR UALA2012042302431](https://openairdocs.org/sdr/UALA2012042302431), Apr 20, 2012: CONNECTOR. UNSECURE. EMERGENCY LIGHT INOPERATIVE ROW 8 TO 12. FOUND LOOSE CONNECTOR. SECURED CONNECTOR. SYSTEM OPS CHECKED NORMAL.
- [SDR UALA2012032301858](https://openairdocs.org/sdr/UALA2012032301858), Mar 23, 2012: FUEL CONTROL. LEAKING. NR 1 ENGINE HAS FUEL LEAK. FUEL LEAKING FROM TOP COVER ON FUEL CONTROL. RMV'D FUEL CONTROL PER AMM. REPLACED FUEL CONTROL.
- [SDR UALA2011110706025](https://openairdocs.org/sdr/UALA2011110706025), Nov 6, 2011: GUARD. OUT OF ADJUST. EMERGENCY EXIT LIGHT SWITCH IN COCKPIT IS VERY TOUCHY, NEEDS ADJUSTMENT. ADJUSTED GUARD ASSY. SYSTEM OP CHECK OK.
- [SDR UALA2011081504333](https://openairdocs.org/sdr/UALA2011081504333), Aug 14, 2011: SKIN. DENTED. EXTERNAL FUSELAGE BETWEEN BS 520 AND BS 540, BETWEEN STR 29L AND STR 28L HAS A DENT. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT THE DAMAGED SKIN AND FABRICATED A RE
- [SDR UALA2011081504298](https://openairdocs.org/sdr/UALA2011081504298), Aug 14, 2011: STRUCTURE. DAMAGED. FUSELAGE DAMAGE AREA OF STA 500, 520 STR 17L,18L ON LEFT SIDE OF FUSELAGE APPROX 10 FT FROM DOOR 1L AT FLOOR LEVEL. MAJOR REPAIR ACCOMPLISHED: INTERIM RPR DONE 
- [SDR UALA2011081504291](https://openairdocs.org/sdr/UALA2011081504291), Aug 13, 2011: FRAME. DAMAGED. MAJOR REPAIR ACCOMPLISHED: FRAME AT BS 1680 RH HAS SMALL CUT IN THE FWD. FACE OF FRAME JUST BELOW FLOORBEAM T-CAP. MAJOR REPAIR ACCOMPLISHED: TRIMMED OUT DAMAGE
- [SDR UALA2011081504290](https://openairdocs.org/sdr/UALA2011081504290), Aug 13, 2011: SKIN. DAMAGED. BS 500 - 520 LT BETWEEN S17-18L HAS INCURRED DAMAGE TO SKIN. MAJOR REPAIR ACCOMPLISHED: FABRICATED REPAIR DOUBLER AND FILLER PER REO G13842, REV. D.
- [SDR UALA2011081504289](https://openairdocs.org/sdr/UALA2011081504289), Aug 13, 2011: STRINGER. DAMAGED. STRINGER 17L FROM BS 500 TO 520 HAS OUT OF ROUND HOLES. MAJOR REPAIR ACCOMPLISHED: R & R STRINGER 17L SECTION FROM BS 476 TO 583 PER REO G13842, REV. D.
- [SDR UALA2011081504272](https://openairdocs.org/sdr/UALA2011081504272), Aug 12, 2011: FRAME. BROKEN. MAIN CABIN STA 520 FRAME AND CHORD IS BROKEN OUT BETWEEN STR 17L AND STR 18L. MAJOR REPAIR ACCOMPLISHED: REMOVED DAMAGED FRAME & CHORD SECTION AND REPLACED FRAM
- [SDR UALA2011081504271](https://openairdocs.org/sdr/UALA2011081504271), Aug 12, 2011: LAMP. INOPERATIVE. RH AFT OVERWING EMERGENCY LIGHT INOPERATIVE. RELAMPED EMERGENCY LIGHT PER MM AND OPS CHECKED GOOD.
- [SDR UALA2011081504270](https://openairdocs.org/sdr/UALA2011081504270), Aug 12, 2011: SWITCH. MISWIRED. EMERGENCY LIGHTS INOPERATIVE. REWIRED EMERGENCY LIGHT SWITCHES PER WDM AND OPS CHECKED GOOD PER MM.
- [SDR UALA2011081504269](https://openairdocs.org/sdr/UALA2011081504269), Aug 12, 2011: SWITCH. MALFUNCTIONED. EMERGENCY ESCAPE LIGHTS DO NOT ILLUMINATE DURING TEST 1 OF THE ELECTRICAL SYSTEM SQUIB AND PRESSURE SWITCH TEST AS FOUND IN AMM AND ROUTINE JIC 5R 25I9050. PERF
- [SDR UALA2011081504263](https://openairdocs.org/sdr/UALA2011081504263), Aug 12, 2011: FLOORBEAM. CORRODED. FLOORBEAM AT BS 1681, RBL 37 - RBL 42 CORRODED. REMOVED DAMAGED TEE ENTIRE LENGTH BETWEEN RBL 60 TO LBL 60. FABRICATED A REPLACEMENT TEE ANGLE AND FILLERS AND A
- [SDR UALA2011081204238](https://openairdocs.org/sdr/UALA2011081204238), Aug 11, 2011: FLOORBEAM. BROKEN. MAIN CABIN FLOORBEAM AT BS 500L IS BROKEN OFF FROM LBL 45 TO THE END OF THE BEAM. REMOVED DAMAGED SECTION OF FLOORBEAM AND FABRICATED A REPLACEMENT FLOORBEAM SE
- [SDR UALA2011081204236](https://openairdocs.org/sdr/UALA2011081204236), Aug 11, 2011: PUSHROD. OUT OF ADJUST. R-4 DOOR FAILED MIDWAY CHECK. ADJUSTED R-4 DOOR GIRT BAR CRANK PUSH RODS PER MM AND DOOR MIDWAY OPS CK GOOD ON NON ROUTINE 21146 BY MECH-110236 AND INSP QC031.

All 121: https://openairdocs.org/aircraft/N571UA/unmatched-reports.md

## STCs that may be installed (OpenAirDocs)

None matched to this aircraft's models.

## Earlier aircraft with N571UA

The FAA can reassign an N-number once a registration is cancelled. These aircraft carried N571UA before.

- [Cancelled 2018-03-20](https://openairdocs.org/deregistered/N571UA-2018-03-20): Boeing 767-300, S/N 27311. Owner: [Unical Aviation Inc](https://openairdocs.org/faa-owner/UNICAL%20AVIATION%20INC), [City Of Industry, CA](https://openairdocs.org/faa-place/CA/City%20Of%20Industry)

## Related

- Other Zipline International P2 ZIP aircraft: https://openairdocs.org/model/zipline-international-p2-zip/aircraft.md

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