# Service difficulty reports: N969Z, cancelled May 5, 2007 A list on [N969Z, cancelled May 5, 2007](https://openairdocs.org/deregistered/N969Z-2007-05-05.md). Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first. - [SDR TWAA9908707](https://openairdocs.org/sdr/TWAA9908707.md): Longeron · cracked · Jun 22, 1999 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > ACCOMPLISHING MC8-AD-AM FOUND THE RT LONGERON FLANGE ON LONGERON 1 CRACKED ONE INCH AT BELT RING STA 642. SPLICED IN NEW LONGERON SECTION PER SRM 53-02, FIG 18. CHECK-C 4-12-99 STL. - [SDR TWAA9906201](https://openairdocs.org/sdr/TWAA9906201.md): Splice · cracked · Apr 9, 1999 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > DURING CHECK-C MAINT, FOUND LONGERON 28L SPLICE AT STA 370, CRACKED AND CORRODED. CRACK.75 IN LONG. INSTALLED REPAIR PER SRM 53-02, FIG 18. - [SDR TWAA9814702](https://openairdocs.org/sdr/TWAA9814702.md): Power Supply · inoperative · Sep 10, 1998 · N969Z · Doug DC915 · Emergency Lighting > FLOOR EGRESS LIGHTS REPORTED INOP ROWS 12 TO 16. REPLACED POWER SUPPLY. CHECK-C 11-22-97 STL. - [SDR TWAA9814318](https://openairdocs.org/sdr/TWAA9814318.md): Intercostal · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > INTERCOASTAL 28R RBL 14 IN AT STA 120 TO 130, REMOVED FOR CORROSION AND CRACK. MADE 9911549-2 FROM 7075-0 AND HEAT TREATED TO T6 CONDITION AND INSTALLED WITH HI-LOKS AND RIVETS. CHECK-C 11-22-97 STL. - [SDR TWAA9814317](https://openairdocs.org/sdr/TWAA9814317.md): Jamb · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > DOOR JAMB STRUCTURE REMOVED AT ELECTRONIC COMPT DOOR FOR CORROSION DAMAGE STA 134 TO 160, LONGERON 28L TO 28R WITH ATTACH STRUCTURE. ACCOMPLISHED ARA 9240 REV A. INSTALLED DOOR JAMB STRUCTURE PER DWG 5910343. CHECK-C 11-22-97 STL. - [SDR TWAA9814316](https://openairdocs.org/sdr/TWAA9814316.md): Angle · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > FORMER FOOT ANGLE LONGERON 26R TO 27R STA 160 REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9911515. CHECK-C 11-22-97 STL. - [SDR TWAA9814315](https://openairdocs.org/sdr/TWAA9814315.md): Angle · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > FORMER FOOT ANGLE LONGERON 26L TO 27L REMOVED FOR CORROSION. REMOVED AND REPLACED FORMER FOOT REF DOUGLAS DWG 9911515. CHECK-C 11-22-97 STL. - [SDR TWAA9814314](https://openairdocs.org/sdr/TWAA9814314.md): Angle · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > CHORD ANGLE REMOVED FOR CORROSION DAMAGE STA 110 TO 129, LBL 14 IN. INSTALLED NEW CHORD ANGLE REF DOUGLAS DWG 5911401. CHECK-C 11-22-97 STL. - [SDR TWAA9814313](https://openairdocs.org/sdr/TWAA9814313.md): Former · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Main, Frame > FORMER RING REMOVED STA 134, LONGERON 24L TO L24R DUE TO CORROSION DAMAGE. INSTALLED NEW FORMER RING REF DOUGLAS DWG 9911512 AND ARA 9240. CHECK-C 11-22-97 STL. - [SDR TWAA9814312](https://openairdocs.org/sdr/TWAA9814312.md): Skin · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Main, Plate/Skin > STA 110 TO 174 BELLY SKIN REMOVED FOR CORROSION DAMAGE FROM LONGERON 26L TO 26R. REMOVED AND REPLACED SKIN PER ARA 9240. CHECK-C 11-22-97 STL. - [SDR TWAA9814311](https://openairdocs.org/sdr/TWAA9814311.md): Skin · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Main, Plate/Skin > DURING ROUTINE MAINT, FOUND CORROSION ON ELECTRONIC COMPT DOOR DOUBLER AND EXTERIOR SKIN AROUND DOOR. REMOVED AND REPLACED SKIN AND DOUBLER PER ARA 9240. CHECK-C 11-22-97 STL. - [SDR TWAA9813419](https://openairdocs.org/sdr/TWAA9813419.md): Longeron · corroded · Sep 2, 1998 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > INTERCOASTAL LONGERON 28L STA 130 TO 160 HAD CORROSION DAMAGE. INSTALLED INTERCOASTAL PER DWG 5910343. COMPLIED WITH ARA 9240 REV A. CHECK-C 11-22-98 STL. - [SDR TWAA9713501](https://openairdocs.org/sdr/TWAA9713501.md): Angle · cracked · Nov 18, 1997 · N969Z · Doug DC915 · Fuselage Miscellaneous Structure > STL - REPAIRED ONE QUARTER INCH CRACK IN VERTICAL STABILIZER TO FUSELAGE ATTACH ANGLE LEFT SIDE AT STATION 910. (M) - [SDR 96ZZZX4911](https://openairdocs.org/sdr/96ZZZX4911.md): Longeron · cracked · Aug 20, 1996 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > STL - DURING O-15, FOUND A.25 INCH CRACK IN LONGERON 13R, STA 768. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES. - [SDR 96ZZZX4910](https://openairdocs.org/sdr/96ZZZX4910.md): Longeron · cracked · Aug 20, 1996 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > STL - DURING OP-15, FOUND A.25 INCH CRACK IN LONGERON 26L, STA 313. REPAIRED PER SRM 53-02, FIGURE 4. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES. - [SDR 96ZZZX4901](https://openairdocs.org/sdr/96ZZZX4901.md): Longeron · cracked · Aug 20, 1996 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > STL - DURING OP-15, FOUND A.25 INCH CRACK IN LONGERON 27L AND.50 INCH CRACK IN OUTBOARD HAT SECTION, STA 313. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 64,463 HOURS; 76,506 CYCLES. - [SDR 96ZZZX4899](https://openairdocs.org/sdr/96ZZZX4899.md): Longeron · cracked · Aug 20, 1996 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > STL - DURING OP-15, FOUND.50 INCH CRACK IN LONGERON 28L, STA 313. REPAIRED PER SRM 53-02, FIGURE 2. AIRCRAFT TOTAL TIME: 63,463 HOURS; 76,506 CYCLES. - [SDR 96ZZZM1335](https://openairdocs.org/sdr/96ZZZM1335.md): Longeron · cracked · Aug 8, 1996 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > STL - DURING OP-15, FOUND.5 INCH CRACK IN RIGHT FLANGE, LONGERON 1, STATION 566. INSTALLED LONGERON REPAIR SPLICE PER SRM 53-02, FIGURE 4. (M) - [SDR 96ZZZM189](https://openairdocs.org/sdr/96ZZZM189.md): Skin · cracked · Dec 30, 1995 · N969Z · Doug DC915 · Fuselage Main, Plate/Skin > STL - DURING SPECIAL CHECK, FOUND ONE AND TWO INCH CRACKS IN FUSELAGE SKIN BETWEEN RIVETS AT STATION 817, LONGERON R9, AND A 1 INCH FUSELAGE SKIN CRACK AT STATION 817, LONGERONS R7-R8. REPAIRED PER SERVICE BULLETIN A53-147, AND DRAWING J060143. (M) - [SDR 95ZZZW739](https://openairdocs.org/sdr/95ZZZW739.md): Longeron · cracked · Apr 17, 1995 · N969Z · Doug DC915 · Fuselage Main, Longeron/Stringer > DURING SPECIAL CHECK, FOUND A TWO INCH CRACK IN LONGERON 19L, STATION 218. REPAIRED PER SRM 53-02. ## 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 = 'N969Z' AND deregistration_id = 'N969Z-2007-05-05' ORDER BY difficulty_date DESC ``` This list as a web page: https://openairdocs.org/deregistered/N969Z-2007-05-05/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.