# Service difficulty reports: N573SH, cancelled Jun 23, 2011 A list on [N573SH, cancelled Jun 23, 2011](https://openairdocs.org/deregistered/N573SH-2011-06-23.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR EE4Y20110133](https://openairdocs.org/sdr/EE4Y20110133.md): Skin · corroded · Feb 28, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > SKIN CORRODED AT STA Y725 BTWN LONG 29R AND LONG 30R. - [SDR EE4Y20110132](https://openairdocs.org/sdr/EE4Y20110132.md): Skin · corroded · Feb 28, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > SKIN CORRODED LOCATED FROM STA Y1155 TO STA Y12111 BTWN LONG 26R AND LONG 28R - [SDR EE4Y20110131](https://openairdocs.org/sdr/EE4Y20110131.md): Skin · corroded · Feb 28, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > SKIN CORRODED LOCATED FROM STA Y180 TO STA Y190 BTWN LONG 29L AND LONG 30 - [SDR EE4Y20110120](https://openairdocs.org/sdr/EE4Y20110120.md): Skin · dented · Feb 25, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE AT STA Y441.5 BTWN LONG 21R AND LONG 22R SKIN DENTED. - [SDR EE4Y20110119](https://openairdocs.org/sdr/EE4Y20110119.md): Skin · damaged · Feb 25, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE AT STA Y257 BTWN LONG 21R AND LONG 22R SKIN WITH BLENDOUT - [SDR EE4Y20110118](https://openairdocs.org/sdr/EE4Y20110118.md): Skin · dented · Feb 25, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE AT STA Y359 BTWN LONG 21R AND LONG 22R SKIN DENTED - [SDR EE4Y20110116](https://openairdocs.org/sdr/EE4Y20110116.md): Skin · dented · Feb 25, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE AT STA Y459 BTWN LONG 21R AND LONG 22R SKIN DENTED - [SDR EE4Y20110117](https://openairdocs.org/sdr/EE4Y20110117.md): Doubler · cracked · Feb 25, 2011 · N573SH · Doug DC982 · Wing, Plate/Skin > DOUBLER CRACKED LOCATED LT WING UPPER SURFACE AT STA XCW110 MLG - [SDR EE4Y20110127](https://openairdocs.org/sdr/EE4Y20110127.md): Longeron · corroded · Feb 23, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > LOWER FUSELAGE AFT CARGO COMPARMENT LONGERON 29LH WITH CORROSIONAT STA Y 1026 - [SDR EE4Y20110126](https://openairdocs.org/sdr/EE4Y20110126.md): Longeron · corroded · Feb 23, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > LOWER FUSELAGE AFT CARGO COMPARMENT LONGERON 30 WITH CORROSION FROM STA Y 1024 TO STA Y 1032 - [SDR EE4Y20110125](https://openairdocs.org/sdr/EE4Y20110125.md): Skin · bulged · Feb 22, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA 216 BETWEEN LONGERONS 18R AND 19R SKIN BULGED. - [SDR EE4Y20110124](https://openairdocs.org/sdr/EE4Y20110124.md): Skin · dented · Feb 22, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE STA 215 BETWEEN LONGERONS 18L AND 19L SKIN DENTED. - [SDR EE4Y20110123](https://openairdocs.org/sdr/EE4Y20110123.md): Skin · bulged · Feb 22, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE AT STA 229 BETWEEN LONGERONS 30 AND 29L SKIN BULGED - [SDR EE4Y20110122](https://openairdocs.org/sdr/EE4Y20110122.md): Skin · dented · Feb 22, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > LOWER FUSELAGE, AT Y STA 359 BETWEEN LONGERONS 21R AND 22R SKIN DENTED. - [SDR EE4Y20110115](https://openairdocs.org/sdr/EE4Y20110115.md): Fitting · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Main, Attach Fittings > 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.md): Fitting · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Main, Attach Fittings > 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.md): Fitting · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > 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.md): Support Fitting · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > REPORTED AT AFT CARGO COMPARTMENT YSTA 1307, -X16, SUPPORT FITTING CORRODED. - [SDR EE4Y2011052](https://openairdocs.org/sdr/EE4Y2011052.md): Skin · dented · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > 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.md): Floorbeam · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Main, Floor Beam > 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.md): Floorbeam · corroded · Feb 17, 2011 · N573SH · Doug DC982 · Fuselage Main, Floor Beam > 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.md): Longeron · corroded · Feb 15, 2011 · N573SH · Doug DC982 · Fuselage Structure (General) > DURING THE INSP FOUND THE LONG 30 CORRODED FROM 1147 TO 1201 IN SEVERAL PARTS. - [SDR EE4Y20110108](https://openairdocs.org/sdr/EE4Y20110108.md): Longeron · corroded · Feb 15, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > DURING THE INSP, FOUND LONG 30 CORRODED FROM 1119 TO 1200. ACTION THE LONG REPAIRED TO EO. - [SDR EE4Y20110107](https://openairdocs.org/sdr/EE4Y20110107.md): Skin · corroded · Feb 15, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > 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.md): Frame · corroded · Feb 14, 2011 · N573SH · Doug DC982 · Fuselage Main, Frame > LOWER FUSELAGE MID CARGO COMPARMENT YSTA 598 BETWEEN LONGERON 27LT AND 27RT FRAME CORRODED. - [SDR EE4Y20110104](https://openairdocs.org/sdr/EE4Y20110104.md): Skin · corroded · Feb 10, 2011 · N573SH · Doug DC982 · Wing, Plate/Skin > 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.md): Longeron · corroded · Feb 9, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > DURING THE INSP, FOUND THE LONGERON 30 CORRODED FROM 1993 TO 1241. - [SDR EE4Y20110102](https://openairdocs.org/sdr/EE4Y20110102.md): Longeron · corroded · Feb 9, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > DURING THE INSP, FOUND THE LONGERON 30 CORRODED FROM 588 TO 664. REPAIRED WITH FAA DER. - [SDR EE4Y20110101](https://openairdocs.org/sdr/EE4Y20110101.md): Doubler · corroded · Feb 9, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > REPORTED MID CARGO COMPARMENT AT Y STA 655, LOWER CUTOUT SKIN AREA, INTERNAL DOUBLER WITH CORROSION. - [SDR EE4Y20110100](https://openairdocs.org/sdr/EE4Y20110100.md): Beam · corroded · Feb 9, 2011 · N573SH · Doug DC983 · Fuselage Main, Structure > REPORTED MID CARGO COMPARTMENT LOWER JAMB BEAM WITH CORROSION AT SEVERAL PLACES. - [SDR EE4Y20110080](https://openairdocs.org/sdr/EE4Y20110080.md): Frame · cracked · Feb 3, 2011 · N573SH · Doug DC982 · Fuselage Main, Frame > UPPER FUSELAGE, OVERWING FRAME WITH ANGLE CRACKED, AT STA 905 +X61 -Z6. REPLACED ANGLE. - [SDR EE4Y20110081](https://openairdocs.org/sdr/EE4Y20110081.md): Frame · cracked · Feb 3, 2011 · N573SH · Doug DC982 · Fuselage Main, Frame > UPPER FUSELAGE, OVERWING FRAME WITH ANGLE CRACKED, AT STA 845 -X -Z6. REPLACED ANGLE. - [SDR EE4Y20110077](https://openairdocs.org/sdr/EE4Y20110077.md): Doubler · corroded · Feb 3, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > 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.md): Doubler · corroded · Feb 2, 2011 · N573SH · Doug DC982 · Fuselage Main, Structure > 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.md): Floor Support · corroded · Jan 28, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > FLOOR SUPPORT CORRODED LOCATED ON MID C/C STA Y598, BTW -X16 AND +X16. - [SDR EE4Y2011051](https://openairdocs.org/sdr/EE4Y2011051.md): Fitting · corroded · Jan 28, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > REPORTED END FITTING CORRODED LOCATED ON MID C/C STA Y820, LONG 29R. - [SDR EE4Y20110034](https://openairdocs.org/sdr/EE4Y20110034.md): Door · delaminated · Jan 24, 2011 · N573SH · Doug DC982 · Wing, Plate/Skin > 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.md): Spar · damaged · Jan 20, 2011 · N573SH · Doug DC982 · Engine Mount Section > THE FRONT SPARS ENGINES 1 AND 2, ENGINE MOUNTING HOLES WITH LIGHT NOTCHES. - [SDR EE4Y20110032](https://openairdocs.org/sdr/EE4Y20110032.md): Skin · dented · Jan 18, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > 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.md): Longeron · corroded · Jan 11, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > 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.md): Longeron · corroded · Jan 11, 2011 · N573SH · Doug DC982 · Fuselage Main, Longeron/Stringer > 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.md): Skin · dented · Jan 11, 2011 · N573SH · Doug DC982 · Fuselage Main, Plate/Skin > REPORT UPPER SKIN WITH DENT AT STA Y52, +Z6, RT SIDE. - [SDR EE4Y20110006](https://openairdocs.org/sdr/EE4Y20110006.md): Support · corroded · Jan 10, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > 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.md): Support Fitting · corroded · Jan 10, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > LOWER FUSELAGE AFT CARGO COMPARMENT YSTA 1250 BETWEEN LONGERON 27RT AND 27LT SUPPORT FITTING CORRODED. - [SDR EE4Y20110004](https://openairdocs.org/sdr/EE4Y20110004.md): Support Fitting · corroded · Jan 10, 2011 · N573SH · Doug DC982 · Fuselage Miscellaneous Structure > (EE4Y) LOWER FUSELAGE AFT CARGO COMPARMENT Y STA 1287 BETWEEN LONGERONS 27 AND 28RT AND BETWEEN LONGERONS 27 AND 28LT SUPPORT FITTING CORRODED. ## The whole list in SQL Runs in DuckDB 1.2 or later on the release's Parquet files over HTTPS: ```sql SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE n_number = 'N573SH' AND deregistration_id = 'N573SH-2011-06-23' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N573SH-2011-06-23/reports --- OpenAirDocs.org is an independent research project of [Contrail Labs](https://contraillabs.com/). It is not affiliated with the FAA or the NTSB. Source documents are U.S. government works in the public domain.