# N573SH: Mcdonnell Douglas DC-9-82, registration cancelled 2011-06-23

- Type: Cancelled registration (FAA registry, deregistered aircraft)
- Cancelled: June 23, 2011
- Exported to: Venezuela
- Status when cancelled: First renewal notice
- Airframe: [Mcdonnell Douglas DC-9-82](https://openairdocs.org/model/mcdonnell-douglas-dc-9-82) (registry code 3022084)
- Data sheets: [TCDS A6WE](https://openairdocs.org/tcds/A6WE) (OpenAirDocs)
- Serial number: 49517
- Type of aircraft: Fixed wing multi engine
- Certificate issued: May 20, 2009
- Last registry action: May 20, 2009
- Mode S code: A75B26
- Owner when cancelled: [Pegasus Aviation IV Inc](https://openairdocs.org/faa-owner/PEGASUS%20AVIATION%20IV%20INC)
- Location: [San Francisco, CA](https://openairdocs.org/faa-place/CA/San%20Francisco)
- Owner type: Corporation
- Owner's area on the map: 37.7984° N, 122.3992° W: Placed by OpenAirDocs at the center of ZIP code 94111, within about a mile (OpenAirDocs). The owner's mailing address, not where the aircraft was based
- The mark today: https://openairdocs.org/aircraft/N573SH
- FAA registry: https://registry.faa.gov/AircraftInquiry/Search/NNumberResult?nNumberTxt=573SH
- Page: https://openairdocs.org/deregistered/N573SH-2011-06-23

From the FAA registry file of October 29, 2026, cancelled registrations. Owners' street addresses are left out. The Mode S code belongs to the N-number, not the airframe.

ADs and bulletins for the Mcdonnell Douglas DC-9-82: https://openairdocs.org/model/mcdonnell-douglas-dc-9-82.md

## Service difficulty reports (45)

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model.

- [SDR EE4Y20110133](https://openairdocs.org/sdr/EE4Y20110133), Feb 28, 2011: SKIN. CORRODED. SKIN CORRODED AT STA Y725 BTWN LONG 29R AND LONG 30R.
- [SDR EE4Y20110132](https://openairdocs.org/sdr/EE4Y20110132), Feb 28, 2011: SKIN. CORRODED. SKIN CORRODED LOCATED FROM STA Y1155 TO STA Y12111 BTWN LONG 26R AND LONG 28R
- [SDR EE4Y20110131](https://openairdocs.org/sdr/EE4Y20110131), Feb 28, 2011: SKIN. CORRODED. SKIN CORRODED LOCATED FROM STA Y180 TO STA Y190 BTWN LONG 29L AND LONG 30
- [SDR EE4Y20110120](https://openairdocs.org/sdr/EE4Y20110120), Feb 25, 2011: SKIN. DENTED. LOWER FUSELAGE AT STA Y441.5 BTWN LONG 21R AND LONG 22R SKIN DENTED.
- [SDR EE4Y20110119](https://openairdocs.org/sdr/EE4Y20110119), Feb 25, 2011: SKIN. DAMAGED. LOWER FUSELAGE AT STA Y257 BTWN LONG 21R AND LONG 22R SKIN WITH BLENDOUT
- [SDR EE4Y20110118](https://openairdocs.org/sdr/EE4Y20110118), Feb 25, 2011: SKIN. DENTED. LOWER FUSELAGE AT STA Y359 BTWN LONG 21R AND LONG 22R SKIN DENTED
- [SDR EE4Y20110116](https://openairdocs.org/sdr/EE4Y20110116), Feb 25, 2011: SKIN. DENTED. LOWER FUSELAGE AT STA Y459 BTWN LONG 21R AND LONG 22R SKIN DENTED
- [SDR EE4Y20110117](https://openairdocs.org/sdr/EE4Y20110117), Feb 25, 2011: DOUBLER. CRACKED. DOUBLER CRACKED LOCATED LT WING UPPER SURFACE AT STA XCW110 MLG
- [SDR EE4Y20110127](https://openairdocs.org/sdr/EE4Y20110127), Feb 23, 2011: LONGERON. CORRODED. LOWER FUSELAGE AFT CARGO COMPARMENT LONGERON 29LH WITH CORROSIONAT STA Y 1026
- [SDR EE4Y20110126](https://openairdocs.org/sdr/EE4Y20110126), Feb 23, 2011: LONGERON. CORRODED. LOWER FUSELAGE AFT CARGO COMPARMENT LONGERON 30 WITH CORROSION FROM STA Y 1024 TO STA Y 1032
- [SDR EE4Y20110125](https://openairdocs.org/sdr/EE4Y20110125), Feb 22, 2011: SKIN. BULGED. LOWER FUSELAGE STA 216 BETWEEN LONGERONS 18R AND 19R SKIN BULGED.
- [SDR EE4Y20110124](https://openairdocs.org/sdr/EE4Y20110124), Feb 22, 2011: SKIN. DENTED. LOWER FUSELAGE STA 215 BETWEEN LONGERONS 18L AND 19L SKIN DENTED.
- [SDR EE4Y20110123](https://openairdocs.org/sdr/EE4Y20110123), Feb 22, 2011: SKIN. BULGED. LOWER FUSELAGE AT STA 229 BETWEEN LONGERONS 30 AND 29L SKIN BULGED
- [SDR EE4Y20110122](https://openairdocs.org/sdr/EE4Y20110122), Feb 22, 2011: SKIN. DENTED. LOWER FUSELAGE, AT Y STA 359 BETWEEN LONGERONS 21R AND 22R SKIN DENTED.
- [SDR EE4Y20110115](https://openairdocs.org/sdr/EE4Y20110115), Feb 17, 2011: FITTING. CORRODED. REPORTED FITTING CORRODED LOCATED AT AFT CARGO COMPT AT STA 1231 BTWN LONG 27R AND LONG 28R. THE FITTING DAMAGED WAS REPLACED.
- [SDR EE4Y20110114](https://openairdocs.org/sdr/EE4Y20110114), Feb 17, 2011: FITTING. CORRODED. REPORTED FITTING CORRODED LOCATED IN THE AFT CARGO COMPT AT STA 1218 BTWN LONG 27R AND LONG 28R. THE FITTING DAMAGED WAS REPLACED.
- [SDR EE4Y20110111](https://openairdocs.org/sdr/EE4Y20110111), Feb 17, 2011: FITTING. CORRODED. REPORTED FITTING CORRODED, LOCATED AT MID C/C AT STA 769 AT +X16. THE FITTING DAMAGED WAS REPLACED.
- [SDR EE4Y20110113](https://openairdocs.org/sdr/EE4Y20110113), Feb 17, 2011: SUPPORT FITTING. CORRODED. REPORTED AT AFT CARGO COMPARTMENT YSTA 1307, -X16, SUPPORT FITTING CORRODED.
- [SDR EE4Y2011052](https://openairdocs.org/sdr/EE4Y2011052), Feb 17, 2011: SKIN. DENTED. LOWER FUSELAGE AT STA 459 BETWEEN LONG 21R AND 22R SKIN DENTED. FUSELAGE REPAIRED IAW MFG DWG SG09530001, VIEW D1, SHEETS 1 AND 3.
- [SDR EE4Y20110112](https://openairdocs.org/sdr/EE4Y20110112), Feb 17, 2011: FLOORBEAM. CORRODED. REPORTED SUPPORT FITTING CORRODED LOCATED AT AFT C/C AT STA Y1174, -X2. THE PART DAMAGED WAS REPLACED.
- [SDR EE4Y20110110](https://openairdocs.org/sdr/EE4Y20110110), Feb 17, 2011: FLOORBEAM. CORRODED. REPORTED SUPPORT TEE CORRODED, LOCATED LOWER FUSELAGE FILLET FAIRING AREA AT STA Y988, BTWN +20 AND -X20. THE SUPPORT TEE DAMAGED WAS REPLACED.
- [SDR EE4Y20110109](https://openairdocs.org/sdr/EE4Y20110109), Feb 15, 2011: LONGERON. CORRODED. DURING THE INSP FOUND THE LONG 30 CORRODED FROM 1147 TO 1201 IN SEVERAL PARTS.
- [SDR EE4Y20110108](https://openairdocs.org/sdr/EE4Y20110108), Feb 15, 2011: LONGERON. CORRODED. DURING THE INSP, FOUND LONG 30 CORRODED FROM 1119 TO 1200. ACTION THE LONG REPAIRED TO EO.
- [SDR EE4Y20110107](https://openairdocs.org/sdr/EE4Y20110107), Feb 15, 2011: SKIN. CORRODED. REPORTED LOWER FUSELAGE FROM YSTA 759.5 TO YSTA 826 AND BETWEEN LONG 27L AND 27R EXTERNAL SKIN WITH CORROSION AT SEVERAL PLACES.
- [SDR EE4Y20110106](https://openairdocs.org/sdr/EE4Y20110106), Feb 14, 2011: FRAME. CORRODED. LOWER FUSELAGE MID CARGO COMPARMENT YSTA 598 BETWEEN LONGERON 27LT AND 27RT FRAME CORRODED.
- [SDR EE4Y20110104](https://openairdocs.org/sdr/EE4Y20110104), Feb 10, 2011: SKIN. CORRODED. DURING THE INSPECTION, WING CTR SECTION, FOUND THE UPPER SKIN BETWEEN XCW 42 AND XCW 58.688 AND BETWEEN STR 6 AND 9 LT SKIN CORRODED.
- [SDR EE4Y20110103](https://openairdocs.org/sdr/EE4Y20110103), Feb 9, 2011: LONGERON. CORRODED. DURING THE INSP, FOUND THE LONGERON 30 CORRODED FROM 1993 TO 1241.
- [SDR EE4Y20110102](https://openairdocs.org/sdr/EE4Y20110102), Feb 9, 2011: LONGERON. CORRODED. DURING THE INSP, FOUND THE LONGERON 30 CORRODED FROM 588 TO 664. REPAIRED WITH FAA DER.
- [SDR EE4Y20110101](https://openairdocs.org/sdr/EE4Y20110101), Feb 9, 2011: DOUBLER. CORRODED. REPORTED MID CARGO COMPARMENT AT Y STA 655, LOWER CUTOUT SKIN AREA, INTERNAL DOUBLER WITH CORROSION.
- [SDR EE4Y20110100](https://openairdocs.org/sdr/EE4Y20110100), Feb 9, 2011: BEAM. CORRODED. REPORTED MID CARGO COMPARTMENT LOWER JAMB BEAM WITH CORROSION AT SEVERAL PLACES.
- [SDR EE4Y20110080](https://openairdocs.org/sdr/EE4Y20110080), Feb 3, 2011: FRAME. CRACKED. UPPER FUSELAGE, OVERWING FRAME WITH ANGLE CRACKED, AT STA 905 +X61 -Z6. REPLACED ANGLE.
- [SDR EE4Y20110081](https://openairdocs.org/sdr/EE4Y20110081), Feb 3, 2011: FRAME. CRACKED. UPPER FUSELAGE, OVERWING FRAME WITH ANGLE CRACKED, AT STA 845 -X -Z6. REPLACED ANGLE.
- [SDR EE4Y20110077](https://openairdocs.org/sdr/EE4Y20110077), Feb 3, 2011: DOUBLER. CORRODED. REPORTED LOWER FUSELAGE MID CARGO COMPARMENT FROM Y STA 598 TO Y STA 617 BETWEEN LONG 29-30 LT INTERNAL DOUBLER WITH CORROSION.
- [SDR EE4Y20110076](https://openairdocs.org/sdr/EE4Y20110076), Feb 2, 2011: DOUBLER. CORRODED. REPORTED LOWER FUSELAGE MID CARGO COMPARMENT FROM Y STA 636 TO Y STA 655 BETWEEN LONG 29-30 LT INTERNAL DOUBLER WITH CORROSION.
- [SDR EE4Y20110052](https://openairdocs.org/sdr/EE4Y20110052), Jan 28, 2011: FLOOR SUPPORT. CORRODED. FLOOR SUPPORT CORRODED LOCATED ON MID C/C STA Y598, BTW -X16 AND +X16.
- [SDR EE4Y2011051](https://openairdocs.org/sdr/EE4Y2011051), Jan 28, 2011: FITTING. CORRODED. REPORTED END FITTING CORRODED LOCATED ON MID C/C STA Y820, LONG 29R.
- [SDR EE4Y20110034](https://openairdocs.org/sdr/EE4Y20110034), Jan 24, 2011: DOOR. DELAMINATED. LT WING T/E BUTE DOOR P/N: 5919572-512 DELAMINATED. DELAMINATED BUTE DOOR WAS REPAIRED BY LOCAL DER.
- [SDR EE4Y20110038](https://openairdocs.org/sdr/EE4Y20110038), Jan 20, 2011: SPAR. DAMAGED. THE FRONT SPARS ENGINES 1 AND 2, ENGINE MOUNTING HOLES WITH LIGHT NOTCHES.
- [SDR EE4Y20110032](https://openairdocs.org/sdr/EE4Y20110032), Jan 18, 2011: SKIN. DENTED. FUSELAGE SKIN DENTED FROM STA Y197.25 TO STA Y200, BTWN LONG 15R AND LONG 16R. DENTED SKIN WAS REPAIRED.
- [SDR EE4Y20110013](https://openairdocs.org/sdr/EE4Y20110013), Jan 11, 2011: LONGERON. CORRODED. REPORT LONGERON 25L CORRODED BTWN STA Y1022 AND STA Y1041. CORRODED LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18
- [SDR EE4Y20110012](https://openairdocs.org/sdr/EE4Y20110012), Jan 11, 2011: LONGERON. CORRODED. REPORT LONGERON 23L CORRODED BTWN STA Y1022 AND STA Y1041. CORRODED LONGERON WAS REPAIRED IAW SRM 53-02, FIG 18.
- [SDR EE4Y2011011](https://openairdocs.org/sdr/EE4Y2011011), Jan 11, 2011: SKIN. DENTED. REPORT UPPER SKIN WITH DENT AT STA Y52, +Z6, RT SIDE.
- [SDR EE4Y20110006](https://openairdocs.org/sdr/EE4Y20110006), Jan 10, 2011: SUPPORT. CORRODED. LOWER FUSELAGE FROM STA 1003 TO 1015 BETWEEN +X15 AND -X15 FILLET FAIRING, ANGLES AND SUPPORTS WITH CORROSION.
- [SDR EE4Y20110005](https://openairdocs.org/sdr/EE4Y20110005), Jan 10, 2011: SUPPORT FITTING. CORRODED. LOWER FUSELAGE AFT CARGO COMPARMENT YSTA 1250 BETWEEN LONGERON 27RT AND 27LT SUPPORT FITTING CORRODED.
- [SDR EE4Y20110004](https://openairdocs.org/sdr/EE4Y20110004), Jan 10, 2011: SUPPORT FITTING. CORRODED. (EE4Y) LOWER FUSELAGE AFT CARGO COMPARMENT Y STA 1287 BETWEEN LONGERONS 27 AND 28RT AND BETWEEN LONGERONS 27 AND 28LT SUPPORT FITTING CORRODED.

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