# Service difficulty reports: N221US, cancelled Jun 14, 2000 A list on [N221US, cancelled Jun 14, 2000](https://openairdocs.org/deregistered/N221US-2000-06-14.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. Page 1 of 2 · 63 reports - [SDR 98ZZZM494](https://openairdocs.org/sdr/98ZZZM494.md): Power Supply · inoperative · May 27, 1998 · N221US · Boeing 7372H5 · Emergency Lighting > FORWARD LEFT (PAX) AND RT SERVICE DOOR EXIT EMERGENCY LIGHTS INOP. REMOVED AND REPLACED FORWARD EMERGENCY LIGHTS POWER SUPPLY PACK, S/N ON 1715, S/N OFF 15002, P/N 60-1321-1, IAW MM 33-51-71. (M) - [SDR 98ZZZM401](https://openairdocs.org/sdr/98ZZZM401.md): Splice · broken · Feb 26, 1998 · N221US · Boeing 7372H5 · Emergency Lighting > ON OVERNIGHT CHECK, FOUND ROW 2 EMERGENCY LIGHT INOP. FOUND BUTT SPLICE BROKEN. REINSTALLED NEW SPLICE, OPS CHECK OK. (M) - [SDR 98ZZZM80](https://openairdocs.org/sdr/98ZZZM80.md): Light · inoperative · Dec 12, 1997 · N221US · Boeing 7372H5 · Emergency Lighting > FORWARD ENTRY DOOR EMERGENCY EXIT LIGHT INOP, FOUND ON RON MAINTENANCE CHECK. REPLACED LIGHT ASSY, OPS CHECK GOOD. (M) - [SDR 97ZZZM426](https://openairdocs.org/sdr/97ZZZM426.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > FOUND 5 CRACKS AT FASTENERS STATION 373, 374, 375, 377, STRINGER 15L. REPAIRED PER SRM 53-30-3. (M) - [SDR 97ZZZM425](https://openairdocs.org/sdr/97ZZZM425.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > FOUND.125 INCH CRACK AT FASTENER HOLE. REPAIRED PER SRM 53-30-1. - [SDR 97ZZZM424](https://openairdocs.org/sdr/97ZZZM424.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > FOUND TWO.25 INCH LONG CRACKS. REPAIRED PER SRM 53-30-3 FIG 1. - [SDR 97ZZZM423](https://openairdocs.org/sdr/97ZZZM423.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > FOUND TWO CRACKS AT FASTENER HOLES. REPAIRED PER SRM 53-30-3. - [SDR 97ZZZM422](https://openairdocs.org/sdr/97ZZZM422.md): Frame · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Frame > FOUND ONE INCH CRACK IN FRAME. REPAIRED PER SRM 51-40-2. - [SDR 97ZZZM421](https://openairdocs.org/sdr/97ZZZM421.md): Frame · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Frame > LEFT OUTBOARD CHORD ANGLE CRACKED STATION 1156 WL 274,.75 INCH CRACK. REPAIRED PER EO 5391G569. - [SDR 97ZZZM420](https://openairdocs.org/sdr/97ZZZM420.md): Stringer · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Longeron/Stringer > ONE INCH CRACK IN STRINGER. REPAIRED PER SRM 53-10-3. - [SDR 97ZZZM419](https://openairdocs.org/sdr/97ZZZM419.md): Skin · disbond · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > SKIN DISBONDED AT LOWER CORNERS OF EMERGENCY EXIT APERTURE, REPAIRED PER EA 42068. - [SDR 97ZZZM418](https://openairdocs.org/sdr/97ZZZM418.md): Skin · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > 3 INCH BY 5 INCH DELAMINATED AREA AND CRACKS AT SIX FASTENER HOLES. REPAIRED PER EA 42062. (M) - [SDR 97ZZZM417](https://openairdocs.org/sdr/97ZZZM417.md): Bulkhead Fitting · cracked · Mar 2, 1997 · N221US · Boeing 7372H5 · Fuselage Main, Bulkhead > BULKHEAD FITTING CRACKED 3 INCHES. TIME LIMITED REPAIR INSTALLED PER EA 42071 AND DWG 65C 29229. (M) - [SDR 96ZZZX1484](https://openairdocs.org/sdr/96ZZZX1484.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > GSO -.1250 INCH CRACK AT RIVET HOLE FOUND. INSTALLED DOUBLER SRM 53-30-3, FIGURE 6. - [SDR 96ZZZX1483](https://openairdocs.org/sdr/96ZZZX1483.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > GSO - FIVE.25 INCH CRACKS AT RIVET HOLES FOUND. INSTALLED REPAIR PER E.A. 40951. - [SDR 96ZZZX1482](https://openairdocs.org/sdr/96ZZZX1482.md): Skin · cracked · Mar 1, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > GSO - 3 CRACKS FORWARD UPPER CORNER, FORWARD SERVICE DOORWAY. INSTALLED DOUBLER PER E.A. 40950. - [SDR E9WA](https://openairdocs.org/sdr/E9WA.md): Skin · damaged · Feb 16, 1996 · N221US · Boeing 7372H5 · Vertical Stabilizer, Plate/Skin > CLT - INSPECTION VISUALLY FOUND MISSING TRAILING EDGE HONEYCOMB CORE MATERIAL LOCATED AT THE VERTICAL STAB AT RUDDER STATION 218 RIGHT TRAILING EDGE PANEL. COMPOSITE REPAIRED AS PER BOEING SRM 51-40-13. (M) - [SDR 96ZZZM798](https://openairdocs.org/sdr/96ZZZM798.md): Skin · damaged · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION FOUND 2 PREVIOUSLY INSTALLED DOUBLERS WITH BLIND FASTENERS LOCATED AT FUSELGE SKIN, FS 727A AT STRINGER 15R AND 16R. INSTALLED EXTERNAL DOUBLER AS PER BOEING SRM 53-30-3 FIG 6 AND USAIR EA NR 24906. (M) - [SDR 96ZZZM744](https://openairdocs.org/sdr/96ZZZM744.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN AT STATION 927-947 AND STRINGER 14L. INSTALLED FIELD FASTENERS AS PER SRM 53-30-3 FIG 17 DETAIL 1. (M) - [SDR 96ZZZM743](https://openairdocs.org/sdr/96ZZZM743.md): Skin · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET.1875 INCH UP AND.125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M) - [SDR 96ZZZM742](https://openairdocs.org/sdr/96ZZZM742.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND STRINGER 15L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 DETAIL 1 FIG 17. (M) - [SDR 96ZZZM741](https://openairdocs.org/sdr/96ZZZM741.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN MEASURING 5 INCHES BY 18 INCHES LOCATED AT STATION 920 TO 927 AND STRINGER 9R TO STRINGER 10R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) - [SDR 96ZZZM740](https://openairdocs.org/sdr/96ZZZM740.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 3 INCHES BY 4 INCHES AT STATION 967 ABOVE STRINGER 5L. INSTALLED FIELD RIVETS AS PER SRM 53-30-3 FIG 17. (M) - [SDR 96ZZZM739](https://openairdocs.org/sdr/96ZZZM739.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 5 INCHES BY 4 INCHES AT STATION 356, STRINGER 15L AND 16L. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 DETAIL I AND TABLE III FIG 17. (M) - [SDR 96ZZZM738](https://openairdocs.org/sdr/96ZZZM738.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND LOCATED AT FUSELAGE SKIN MEASURING 14 INCHES BY 2.5 INCHES AT STATION 902 TO 914 AND STRINGER 13R TO STRINGER 14R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3. (M) - [SDR 96ZZZM737](https://openairdocs.org/sdr/96ZZZM737.md): Skin · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND AND VERIFIED WITH HFEC A 1.25 INCH CRACK LOCATED AT FUSELAGE SKIN FS 1137 AND STRINGER 12L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3 FIG 30. (M) - [SDR 96ZZZM736](https://openairdocs.org/sdr/96ZZZM736.md): Support Beam · corrosion · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure > CLT - INSPECTION VISUALLY FOUND LEVEL I CORROSION AT THE FUSELAGE FLOOR SUPPORT BEAM LOCATED AT LBL 2 TO LBL 6 AND STATION 1014. FABRICATED REPLACEMENT H-CHANNEL AND ATTACH ANGLE AS PER BOEING SRM 51-00-02. (M) - [SDR 96ZZZM735](https://openairdocs.org/sdr/96ZZZM735.md): Skin · gouged · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND A 1.5 INCH GOUGE.019 DEEP AT FUSELAGE SKIN LOCATED AT FS 360 1 INCH ABOVE STRINGER 18L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-3, FIG 28. (M) - [SDR 96ZZZM734](https://openairdocs.org/sdr/96ZZZM734.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER AT THE FUSELAGE SKIN LOCATED AT STATION 927 TO 947 AND STRINGER 21R TO STRINGER 20R. REMOVED AND REPLACED SKIN DOUBLER AS PER BOEING SRM 53-30-3 FIG 17. (M) - [SDR 96ZZZM733](https://openairdocs.org/sdr/96ZZZM733.md): Skin · corrosion · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND A LEVEL I CORRODED PRODUCTION STRINGER SPLICE 6 INCHES AT THE FUSELAGE SKIN LOCATED AT STATION 908 AND STRINGER 20R. REPLACED AND REPAIR STRINGER PRODUCTION SPLICE AS PER BOEING SRM 51-00-00. (M) - [SDR 96ZZZM732](https://openairdocs.org/sdr/96ZZZM732.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND 6 INCH DISBONDED FUSELAGE SKIN LOCATED AT STATION 954 BETWEEN STRINGER 24 AND STRINGER 23R. REPLACED SKIN AS PER USAIR EA NR 58009 AND JOB CARD JZ-57-53500 C-1. (M) - [SDR 96ZZZM731](https://openairdocs.org/sdr/96ZZZM731.md): Angle · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure > CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. INSTALLED AND MANUFACTURED ANGLE AS PER BOEING SRM 20-30-06. (M) - [SDR 96ZZZM730](https://openairdocs.org/sdr/96ZZZM730.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCHES BY 6 INCHES AND 8 INCHES BY 2 INCHES AREAS OF SKIN AND DOUBLER DISBOND LOCATED AT THE FUSELAGE SKIN BETWEEN STATION 277 AND 294.5, STRINGER 5R AND STRINGER 8R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-3 - [SDR 96ZZZM729](https://openairdocs.org/sdr/96ZZZM729.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND STRINGER 10L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 FIG 17. (M) - [SDR 96ZZZM728](https://openairdocs.org/sdr/96ZZZM728.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 312-344 AND STRINGER 5R AND STRINGER 6R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG 17 DETAILES I A - [SDR 96ZZZM727](https://openairdocs.org/sdr/96ZZZM727.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3, FIG 17. (M) - [SDR 96ZZZM726](https://openairdocs.org/sdr/96ZZZM726.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCH BY 2 INCH LOCATED AT STATION 986.5 TO 1016, STRINGER 9R TO STRINGER 10R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3, DETAIL I, FIG 17. (M) - [SDR 96ZZZM725](https://openairdocs.org/sdr/96ZZZM725.md): Chord · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure > CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT A CRACK APPROXIMATELY 1 INCH LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD CHORD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M) - [SDR 96ZZZM724](https://openairdocs.org/sdr/96ZZZM724.md): Vertical Fin · dented · Feb 16, 1996 · N221US · Boeing 7372H5 · Vertical Stabilizer, Plate/Skin > CLT - INSPECTION VISUALLY FOUND A DENT LOCATED AT VERTICAL STABILIZER MEASURING 1 INCH BY 2.5 INCH AT FIN STATION 209.90, RIGHT INSPAR. CUT OUT DAMAGE, INSTALLED DOUBLER AS PER USAIR EA NR 40708. (M) - [SDR 96ZZZM723](https://openairdocs.org/sdr/96ZZZM723.md): Chord · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure > CLT - INSPECTION FOUND BY ULTRASONIC AND EDDY CURRENT, A CRACK APPROXIMATELY 1 INCH, LOCATED AT THE FUSELAGE CHORD, RHS BS 727, OUTBOARD AT STRINGER 18A. CHORD SECTION REPLACED AS PER EO 5394G068, EO 5394G6075 AND SB 737-53-1088. (M) - [SDR 96ZZZM722](https://openairdocs.org/sdr/96ZZZM722.md): Angle · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Miscellaneous Structure > CLT - INSPECTION VISUALLY FOUND A 1.5 INCH CRACK LOCATED AT THE FUSELAGE RADIUS OF ANGLE AT FS 1085 AND STRINGER 2L. INSTALLED AND MANUFACTURED ANGLE AS PER BOEING SRM 20-30-06. (M) - [SDR 96ZZZM721](https://openairdocs.org/sdr/96ZZZM721.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND TWO 6 INCH BY 6 INCH AND 8 INCH BY 2 INCH AREAS OF SKIN AND DOUBLER DISBOND LOCATED AT THE FUSELAGE SKIN BETWEEN STATION 277 AND 294.5, STRINGER 5R AND STRINGER 8R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG - [SDR 96ZZZM720](https://openairdocs.org/sdr/96ZZZM720.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 927 TO 947, STRINGER 9L AND STRINGER 10L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 FIG 17. (M) - [SDR 96ZZZM719](https://openairdocs.org/sdr/96ZZZM719.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND TWO AREAS OF DISBOND, 14 INCHES BY 8 INCHES AND 4 INCHES BY 8 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 312-344 AND STRINGER 5R AND STRINGER 6R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3 FIG 17, DETAILS I A - [SDR 96ZZZM718](https://openairdocs.org/sdr/96ZZZM718.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC FOUND FUSELAGE SKIN AND DOUBLER DISBOND LOCATED AT STATION 635, STRINGER 8R AND STRINGER 9R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3, FIG 17. (M) - [SDR 96ZZZM717](https://openairdocs.org/sdr/96ZZZM717.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND 7 INCHES BY 2 INCHES LOCATED AT STATION 986.5 TO 1016, STRINGER 9R TO STRINGER 10R. INSTALLED FIELD FASTENERS AS PER BOEING SRM 53-30-3, DETAIL I, FIG 17. (M) - [SDR 96ZZZM716](https://openairdocs.org/sdr/96ZZZM716.md): Skin · disbond · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND FUSELAGE SKIN AND DOUBLER DISBOND, 13 INCHES BY 13 INCHES LOCATED AT STATION 986.5 TO 1016 AND STRINGER 12R TO STRINGER 13R. INSTALLED FIELD RIVETS AS PER BOEING SRM 53-30-3 FIG 17 DETAIL I. (M) - [SDR 96ZZZM715](https://openairdocs.org/sdr/96ZZZM715.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC, FOUND SKIN AND DOUBLER DISBOND MEASURING 12 INCHES BY 2.5 INCHES LOCATED FUSELAGE SKIN AT STATION 927-947 AND STRINGER 14L. INSTALLED FIELD FASTENERS AS EPR SRM 53-30-3 FIG 17, DETAIL 1. (M) - [SDR 96ZZZM714](https://openairdocs.org/sdr/96ZZZM714.md): Skin · cracked · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION VISUALLY FOUND A CRACK THROUGH RIVET.1875 INCH UP AND.125 INCH DOWN LOCATED AT FUSELAGE SKIN AT STATION 251 AND STRINGER 11L. INSTALLED DOUBLER AS PER BOEING SRM 53-30-03 AND USAIR EO NR 22870. (M) - [SDR 96ZZZM713](https://openairdocs.org/sdr/96ZZZM713.md): Skin · disbonded · Feb 16, 1996 · N221US · Boeing 7372H5 · Fuselage Main, Plate/Skin > CLT - INSPECTION BY ULTRASONIC FOUND DISBONDED SKIN AND DOUBLER MEASURING 9 INCHES BY 5 INCHES LOCATED AT THE FUSELAGE SKIN AT STATION 288, STRINGER 14L AND STRINGER 15L. INSTALLED FIELD DOUBLERS AS PER BOEING SRM 53-30-3 DETAIL 1 FIG 17. (M) Next page: https://openairdocs.org/deregistered/N221US-2000-06-14/reports.md?page=2 ## 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 = 'N221US' AND deregistration_id = 'N221US-2000-06-14' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N221US-2000-06-14/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.