# Service difficulty reports: N995Z, cancelled Mar 21, 2013

A list on [N995Z, cancelled Mar 21, 2013](https://openairdocs.org/deregistered/N995Z-2013-03-21.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 · 67 reports

- [SDR ZW0A0100901](https://openairdocs.org/sdr/ZW0A0100901.md): Wheel · failed · Apr 27, 2001 · N995Z · Doug DC932 · Wheel/Ski/Float
  > DURING LANDING THE LEFT LANDING GEAR INBD WHEEL RIM FAILED. SOME METAL SEPARATED AND THE TIRE ROLLED OFF THE RIM DAMAGING SOME AREAS OF THE GEAR INCLUDING THE GEAR WIRE HARNESS. CHECK-C 1-20-01 STL.
- [SDR TWAA0101602](https://openairdocs.org/sdr/TWAA0101602.md): Battery Pack · discharged · Jan 21, 2001 · N995Z · Doug DC932 · Emergency Lighting
  > THE EMERGENCY CABIN LIGHTS AT THE LEFT NUMBER 1 CABIN DOOR, RT NUMBER 1, AND COCKPIT DOORS CAME ON WHEN THE SWITCH IS ARMED. REPLACED THE BATTERY PACK. CHECK-C 1-2-01 STL.
- [SDR TWAA0101301](https://openairdocs.org/sdr/TWAA0101301.md): Battery Pack · discharged · Jan 21, 2001 · N995Z · Doug DC932 · Emergency Lighting
  > THE CABIN EMERGENCY LIGHTS AT THE LEFT SIDE NUMBER 1 DOOR, RT SIDE NUMBER 1 DOOR, AND COCKPIT DOOR WERE ON WITH THE SWITCH IN ARM POSITION. REPLACED THE BATTERY PACK. CHECK-C 1-2-01 STL.
- [SDR TWAA0101017](https://openairdocs.org/sdr/TWAA0101017.md): Longeron · cracked · Jan 11, 2001 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, LONGERON 2R WAS CRACKED AT FORMER RING AT STA 658. FOUND DURING VISUAL INSPECTION FOR MC8-AD-AM. REPLACED CRACKED SECTION OF LONGERON AND SPLICED NEW SECTION PER SRM 53-02 PAGE 48.
- [SDR TWAA0101016](https://openairdocs.org/sdr/TWAA0101016.md): Longeron · cracked · Jan 11, 2001 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, LONGERON 5L WAS CRACKED AT FORMER RING AT STA 737. FOUND DURING VISUAL INSPECTION FOR MD8-AD-AM. INSTALLED NEW SECTION OF LONGERON AND MANUFACTURED NEW SPLICE AND INSTALLED SPLICE ON SAID LONGERON PER SRM 53-02 PAGE 5, FIG 3.
- [SDR TWAA0003604](https://openairdocs.org/sdr/TWAA0003604.md): Door Latch · unsecure · Mar 4, 2000 · N995Z · Doug DC932 · Accessory Compartment Doors
  > FWD ACC COMPT DOOR LIGHT ILLUMINATED AT LIFT OFF.. FOUND R LATCH LOOSE ON FWD ACC DOOR NEAREST LIGHT SWITCH. SECURED LATCH. CC00 11-11-99 STL.
- [SDR TWAA0101020](https://openairdocs.org/sdr/TWAA0101020.md): Longeron · cracked · Jan 18, 2000 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING CHECK-C MAINT, LONGERON 3R WAS CRACKED AT FORMER RING STA 639. INSTALLED NEW LONGERON SECTION AND SPLICE PER SRO9530128.
- [SDR TWAA9915203](https://openairdocs.org/sdr/TWAA9915203.md): Skin · cracked · Nov 8, 1999 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING CHECK-C MAINT, FOUND 2 CRACKS IN SKIN IN FWD UPPER CORNER OF THE RT SIDE FORWARD CABIN SERVICE DOOR JAM. CRACKS WERE.0625 IN AND.3125 IN LONG COMING OUT OF RIVETS, AND EDDY CURRENT SHOWED A CRACK THAT WAS UNDER.0625 INCHES IN LENGTH. CUT OUT CRACK
- [SDR TWAA9915103](https://openairdocs.org/sdr/TWAA9915103.md): Skin · cracked · Nov 4, 1999 · N995Z · Doug DC932 · Cargo/Baggage Doors
  > DURING CHECK-C MAINT, TWO SKIN CRACKS WERE FOUND ON THE FORWARD CARGO DOOR, LOWER AFT CORNER, FUSELAGE STA 427 AND LONGERON 27R. CRACKS WERE 13/32 AND 5/32 IN LONG. REPAIRED PER SRM 53-05, FIG 105.
- [SDR TWAA9915001](https://openairdocs.org/sdr/TWAA9915001.md): Doubler · cracked · Nov 3, 1999 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND 3 CRACKS IN INTERNAL SKIN DOUBLER AT FWD ENTRY DOOR CUTOUT. CRACKS WERE 3 INCHES, 1.75 IN, AND.75 IN. REMOVED DAMAGED MATERIAL AND INSTALLED REPAIR PER SRM 53-05, FIG 25A AND ARA 16407.
- [SDR TWAA9914905](https://openairdocs.org/sdr/TWAA9914905.md): End Cap · cracked · Nov 2, 1999 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING CHECK-C MAINT, FOUND LONGERONS R2 AND L2 WITH THE END CAPS CRACKED AT STA 1076, EACH WITH APPROXIMATELY A 1.5 INCH CRACK. REPLACED EACH LONGERON SECTION PER SRM 53-02, FIG 8.
- [SDR TWAA9904402](https://openairdocs.org/sdr/TWAA9904402.md): Battery Pack · discharged · Mar 23, 1999 · N995Z · Doug DC932 · Emergency Lighting
  > THE CABIN EGRESS LIGHTS WERE FOUND INOPERATIVE FROM SEAT ROW 16 TO 21. REPLACED BATTERY PACK. CHECK-C 8-31-98 MCI.
- [SDR TWAA9813207](https://openairdocs.org/sdr/TWAA9813207.md): Bulkhead Jamb · damaged · Aug 13, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING CHECK-C MAINT, AN INTERIM REPAIR WAS FOUND ACCOMPLISHED WITH BLIND FASTENERS ON A CRACK AT THE AFT PRESS BLKHD DOOR JAMB, RT SIDE. INSTALLED DOOR JAMB PERMANENT REPAIR PER ARA 15365 AND SRM 53-05 FIG 30.
- [SDR TWAA9812506](https://openairdocs.org/sdr/TWAA9812506.md): Doubler · corroded · Aug 3, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND REINFORCING DOUBLER ABOVE JACK PAD ABOVE SKIN WITH CORROSION, FS 996 LONGERON 28L TO L28R. REMOVED DOUBLER FOR REPLACEMENT PER SRM 51-01, PG 1 ITEM C. INSTALLED NEW 991561-73 DOUBLER PER DOUGLAS BLUEPRINT NR 9915561 AND SRM 53
- [SDR TWAA9812504](https://openairdocs.org/sdr/TWAA9812504.md): Bulkhead Angle · corroded · Aug 3, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND CORROSION ON L-ANGLE AT PRESSURE BULKHEAD UNDER REPAIR 6 IN LBL TO 6 IN RBL. REMOVED L-ANGLE DOUBLER NR 9915661-33 FOR REPLACEMENT PER SRM 51-10-01, PG 1 ITEM C. INSTALLED NEW L-ANGLE DOUBLER 9915561-33 PER SRM 51-30-2.
- [SDR TWAA9812514](https://openairdocs.org/sdr/TWAA9812514.md): Skin · corroded · Jul 29, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND FUSELAGE CORROSION CLEAN UP BEYOND MANUAL LIMITS, 30 PERCENT REMOVED, AT FS 993, LONGERON 29L ON FUSELAGE SKIN. REPAIRED DAMAGED AREA BY BLENDING OUT AREA AND INSTALLING A DOUBLER PER SRM 53-04, FIG 38 PAGE 209, CONDITION 3.
- [SDR TWAA9812513](https://openairdocs.org/sdr/TWAA9812513.md): Skin · corroded · Jul 29, 1998 · N995Z · Doug DC932 · Service Doors
  > DURING OP 16 MAINT CHECK, FOUND ON LOWER FUSELAGE CORROSION AND FASTENER HEADS MISSING AT LOWER FWD CORNER OF THE AFT LAV DUMP SERVICE DOOR. CUT OUT CORRODED MATERIAL FOR REPAIR PER ACFT SRM 51-10-03. REPAIRED PER ARA 15367 PAGE 1 OF 1.
- [SDR TWAA9812507](https://openairdocs.org/sdr/TWAA9812507.md): Skin · cracked · Jul 26, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND SKIN CRACKED AT STA 192, STR 22L,.1875 IN LONG AT 10 O'CLOCK. REMOVED CRACK PER SRM 53-04, P33 NOTE NR 1. INSTALLED REPAIR PER MO 71N61 PHASE A.
- [SDR TWAA9812119](https://openairdocs.org/sdr/TWAA9812119.md): Skin · cracked · Jul 23, 1998 · N995Z · Doug DC932 · Wing, Plate/Skin
  > DURING OP 16 MAINT CHECK, ON RT WING UPPER SURFACE WING SKIN FOUND CRACK AT O/B AFT CORNER OF FUEL TANK ACCESS PLATE NR 1410A. STOP DRILLED CRACK, INSTALLED DOUBLER PER DRW 5951593RE. ACCOMP NDT CRACK CONTAINMENT CHECK PER 51-00-03.
- [SDR TWAA9812118](https://openairdocs.org/sdr/TWAA9812118.md): Floor · cracked · Jul 23, 1998 · N995Z · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINT CHECK, FOUND RT CENTER CABIN FLOOR PANEL AT FS 465 TO 579 WITH 5 CRACKS AT U-CHANNELS ON BOTTOM SIDE, NR 39 PANEL. NEW PANEL FABRICATED PER SSRM 53-00-104.
- [SDR TWAA9812117](https://openairdocs.org/sdr/TWAA9812117.md): Longeron · cracked · Jul 23, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK LONGERON 23L HAD 1.5 IN CRACK IN O/B FLANGE RUNNING DOWN INTO RADIUS AT FS 200. CONFIRMED BY EDDY CURRENT. REMOVED CRACKED LONG, INSTALLED NEW LONG FROM FACTORY SPLICE TO FACTORY SPLICE, INSTALLED FASTENERS PER SRM 51-30-0 AND 51-30-
- [SDR TWAA9812116](https://openairdocs.org/sdr/TWAA9812116.md): Bulkhead Chord · corroded · Jul 22, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND AT FS 604, THE AFT BULKHEAD OF THE FWD CARGO COMPT, THE BOTTOM CHORD AT STA 30 HAD AREA OF CORROSION. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-03, FIG 10 ITEM 503.
- [SDR TWAA9812115](https://openairdocs.org/sdr/TWAA9812115.md): Tie · corroded · Jul 22, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND STRINGER END TIE CORRODED AT STA 994, STR 27R AND 28R. REMOVED AND REPLACED 2 (P/N 4912515-1), INSTALLED FASTENERS PER SRM 51-30-2 AND 51-30-05.
- [SDR TWAA9812121](https://openairdocs.org/sdr/TWAA9812121.md): Skin · corroded · Jul 21, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND AT BOTTOM OF FUSELAGE SKIN AT FWD END OF RT WHEEL WELL, CORROSION THRU WHERE HINGE PIN SHIELD COVERS. REMOVED CORROSION PER SRM 51-10-03. REPAIRED PER SRM 53-04, FIG 38. REINSTALLED BATH TUB FITTING AND RELATED PARTS PER SRM
- [SDR TWAA9812120](https://openairdocs.org/sdr/TWAA9812120.md): Bulkhead · corroded · Jul 21, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND CORROSION AT BOTTOM OF AFT PRESSURE BULKHEAD, 6 IN LBL TO 6 IN RBL. REMOVED CORROSION BY CUTTING OUT CORRODED SECTION PER SRM 53-03, FIG 9 PAGE 12B. INSTALLED DOUBLER PER SRM 53-03, FIG 9.
- [SDR TWAA9812124](https://openairdocs.org/sdr/TWAA9812124.md): Intercostal · corroded · Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND INTERCOSTAL AT 29R BADLY CORRODED AT STA 965 TO 980. MADE NEW PER SRM 51-01, FABRICATED INTERCOSTAL FROM 7075-0 AND HEAT TREATED PER SRM 53-11-3 PAGE 108. REMOVED CORROSION BY REPLACING INTERCOSTAL PER SRM 51-01, PAGE 1 ITEM C
- [SDR TWAA9812123](https://openairdocs.org/sdr/TWAA9812123.md): Doubler · misinstalled · Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINT CHECK, FOUND REPAIR INSTALLED WITH BLIND FASTENERS ON FUSELGE SKIN AND NO DOUBLER AT STA 965 AND 970 BETWEEN LONG 16L AND 17L. REPLACED BLIND FASTENERS AND INSTALLED FINGER DOUBLER PER SRM 53-04, PAGE 93.
- [SDR TWAA9812122](https://openairdocs.org/sdr/TWAA9812122.md): Longeron · cracked · Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINT CHECK, FOUND LONGERON 17L CRACKED AT STA 965. REPLACED SECTION OF LONGERON FROM FS 955 TO 996, PER SRM 51-10, PG 1 ITEM C, AND INSTALLED LONGERON SPLICE PER SRM 53-02, FIG 18.
- [SDR TWAA9812005](https://openairdocs.org/sdr/TWAA9812005.md): Bulkhead Web · cracked · Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND BULKHEAD 965 RBL 58, APPROX 28 IN ABOVE FLOOR LINE WITH CRACK IN WEB. STOP DRILLED AND INSTALLED DOUBLER. INSTALLED NEW WEB PER MO 72J15, PHASE K, PER DRAWING 4709532 REV A, AND 5936993 REV D.
- [SDR TWAA9812004](https://openairdocs.org/sdr/TWAA9812004.md): Bulkhead Doubler · corroded · Jul 20, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINT CHECK, FOUND SPAR WEB DOUBLER ON AFT SIDE OF BULKHEAR WEB, STA 965 RT SIDE, CRACKED. REPAIRED WITH.090 DOUBLER 2024-T3 AND INSTALLED PER MO 72J15, PHASE K AND DAC DRAWING 4709532 AND 5936993.
- [SDR TWAA9812302](https://openairdocs.org/sdr/TWAA9812302.md): Former · corroded · Jul 17, 1998 · N995Z · Doug DC932 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND FORMER CORRODED AT INBD ANGLE STA 1038, BETWEEN S15R AND S17R. CORROSION GROUND TO A DEPTH OF.090. REMOVED CORROSION PER SRM 51-10-3. REPAIRED FORMER 1038 PER ARA 15366A. INSTALLED FORMER 2014-T6 L ANGLE WITH HI-LOCKS.
- [SDR TWAA9812003](https://openairdocs.org/sdr/TWAA9812003.md): Frame · corroded · Jul 15, 1998 · N995Z · Doug DC932 · Fuselage Main, Frame
  > DURING OP 16 MAINT CHECK, FOUND CORROSION AT STA 965, FORMER S29L TO S29R. SPLICE REPAIRED FORMER PER SRM 53-03, FIG 2A.
- [SDR TWAA9812002](https://openairdocs.org/sdr/TWAA9812002.md): Skin · cracked · Jul 15, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINT CHECK, FOUND A CRACK IN FUSELAGE SKIN LEFT SIDE JUST BELOW THE LEFT PYLON STA 965. AREA HAD AN INTERIM REPAIR WITH BLIND FASTENERS. ACCOMP EDDY CURRENT AND NO CRACKS FOUND, REF 51-00-03. INSTALLED DOUBLER PER SRM 53-04, PAGE 93.
- [SDR TWAA9811909](https://openairdocs.org/sdr/TWAA9811909.md): Longeron · corroded · Jul 15, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 24L WITH INNER GRANULAR CORROSION ON ATTACH FITTING AT FWD SIDE OF FS 996. REMOVED CORROSION PER SRM 51-10-03, STEP 35, PAGE 21. ALODINED AND PRIMED PER TWA STD PROCEDURES. INSTALLED NEW ATTACH FITTING PER SRM
- [SDR TWAA9811908](https://openairdocs.org/sdr/TWAA9811908.md): Bulkhead Clip · cracked · Jul 13, 1998 · N995Z · Doug DC932 · Fuselage Main, Bulkhead
  > DURING OP 16 MAINTENANCE CHECK, FOUND 2 INCH CRACK ON STA 1143 CANTED BULKHEAD WEB CLIP, RT SIDE A RUDDER TRIM CABLE CUT-OUT. REPLACED CRACKED ANGLE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9811907](https://openairdocs.org/sdr/TWAA9811907.md): Intercostal · cracked · Jul 13, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > DURING OP 16 MAINTENANCE CHECK, FOUND INTERCOSTAL AT STA 513 ABOVE S27R CRACKED. REPAIRED PER SRM 53-01, PG 10. INSTALLED DOUBLER REPAIR. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9811903](https://openairdocs.org/sdr/TWAA9811903.md): Longeron · cracked · Jul 13, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29R CRACKED JUST FORWARD ON STATION 587 FRAME. REMOVED AND REPLACED LONGERON END PER DWG INST 592176 PER SRM 51-01 PAG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER DOUGLAS INST DWG 592176 AND SRM 51-60-0. (M)
- [SDR TWAA9811906](https://openairdocs.org/sdr/TWAA9811906.md): Skin · corroded · Jul 10, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > DURING OP 16 MAINTENANCE CHECK, FOUND SKIN PILLOWING AT FS 575 TO FS 604, L27R THROUGH LONGERON 27L. REMOVED FRAMES FROM FS 579 TO FS 604. REMOVED LONGERONS 26L TO 26R. REMOVED DOUBLERS, BLASTED PARTS PER SRM 51-10-03, ITEM 35D. REPLACED DOUBLER FROM STA 5
- [SDR TWAA9811905](https://openairdocs.org/sdr/TWAA9811905.md): Longeron · cracked · Jul 10, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 30 CRACKED JUST FORWARD OF STA 578 FRAME. INSTALLED NEW LONGERON END PER INSTL DWG 592176 PER SRM 51-01, PG 1 ITEM C. INSTALLED WITH NEW FASTENERS PER SRM 51-60-0 AND INSTL DWG 592176. ACFT TT: 77,210 HOURS. A
- [SDR TWAA9811904](https://openairdocs.org/sdr/TWAA9811904.md): Longeron · cracked · Jul 10, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > DURING OP 16 MAINTENANCE CHECK, FOUND LONGERON 29L CRACKED JUST FORWARD OF STA 578 FRAME. REMOVED AND REPLACED LONGERON END PER INSTL DWG 592176 PER SRM 51-01, ITEM C. INSTALLED NEW STRINGER PER INSTL DWG 592176 AND SRM 51-60-0. ACFT TT: 77,210 HOURS. ACF
- [SDR TWAA9811902](https://openairdocs.org/sdr/TWAA9811902.md): Floor Panel · cracked · Jul 8, 1998 · N995Z · Doug DC932 · Fuselage Floor Panel
  > DURING OP 16 MAINTENANCE CHECK, FOUND FORWARD CABIN FLOOR PANEL NR 40 WITH HAT SECTIONS CRACKED IN SEVERAL PLACES. REPLACED CRACKED HAT SECTIONS IN FLOOR PANEL NR 40 PER SRM 53-00-104, PAGE 201 FIG 201. (M)
- [SDR TWAA9811003](https://openairdocs.org/sdr/TWAA9811003.md): Rib · bent · Jul 7, 1998 · N995Z · Doug DC932 · Trailing Edge Flaps
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON LT WING FLAP, TWO RIBS INSIDE LOWER INBD ACCESS PLATE WERE BENT. INSTALLED REPAIR DOUBLER PER ARA 15361. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9810712](https://openairdocs.org/sdr/TWAA9810712.md): Frame · cracked · Jul 1, 1998 · N995Z · Doug DC932 · Fuselage Main, Frame
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOND FORMER FOOT STA 980 CRCKED BELOW LONGEORN 14R AND ABOVE 16R. REPLACED FORMER PER MO 72J14. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9810613](https://openairdocs.org/sdr/TWAA9810613.md): Casting · corroded · Jun 25, 1998 · N995Z · Doug DC932 · Wing, Control Surface Attach Fittings
  > MCI - DURING OP 16 MAINTENANCE CHECK FOUND ON RT WING, THE CENTER AND INBD FWD FLAP HINGE CASTING HAD BADLY PITTED MOUNT HOLES. INSTALLED NEW FLAP HINGE CASTING PER MM 57-40-01, PG 201 TO PG 205. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9810804](https://openairdocs.org/sdr/TWAA9810804.md): Splice · cracked · Jun 24, 1998 · N995Z · Doug DC932 · Leading Edge Devices
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND ON RT WING A CRACK IN WING L.E. ON SPLICE DOUBLER. LOCATED OTBD END OF NR 1 SLAT. INSTALLED SPLICE PER SRM 51-01, PG 1 ITEM C. ACFT TT: 77,210 HOURS. ACFT TC: 84,221. (X)
- [SDR TWAA9810611](https://openairdocs.org/sdr/TWAA9810611.md): Skin · cracked · Jun 22, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP16 MAINTENANCE CHECK, EDDY CURRENT INDICATED.125 INCH LONG CRACK RUNNING AFT FROM UNDER RIVET RBL 13 IN, STATION 699, TOP FUSELAGE SKIN. ACCOMP HFEC PER SRM 51-00-2 FOR CRACK CONTAINMENT. NO CRACK INDICATED. REPAIRED PER DAC REWORK DRAWING S
- [SDR TWAA9810612](https://openairdocs.org/sdr/TWAA9810612.md): Longeron · cracked · Jun 19, 1998 · N995Z · Doug DC932 · Fuselage Main, Longeron/Stringer
  > MCI - DURING OP16 MAINTENANCE CHECK, FOUND FWD ENTRY DOOR AREA LONGERON CRACKED AT STATION 200, L2L. REMOVED CRACKED LONGERON. INSTALLED NEW LONGERON PER SRM 51-06, PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-05. (M)
- [SDR TWAA9810806](https://openairdocs.org/sdr/TWAA9810806.md): Doubler · corroded · Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND DOUBLER AT RBL 58, FLOOR LINE, CORRODED AT STA 929 TO STA 945. REMOVED CORROSION PER 51-10-03, PARA 30 TO PARA 42. REPAIRED PER SRM 53-01, PG 9. INSTALLED NEW DOUBLER. ACFT TT: 77,210 HOURS. ACFT TC: 84,221.
- [SDR TWAA9810609](https://openairdocs.org/sdr/TWAA9810609.md): Skin · cracked · Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Main, Plate/Skin
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND CRACK AT SEVENTH FASTENER ABOVE LAP SEAM, LONGERON 14, AT FS 1076 ABOVE RT ENGINE PYLON. CRACK IN BEYOND STOP DRILL, UNDER PREVIOUS REPAIR. CUT OUT CRACK AND INSTALLED DOUBLER PER SRM 53-04, FIG 18. (M)
- [SDR TWAA9810608](https://openairdocs.org/sdr/TWAA9810608.md): Angle · cracked · Jun 18, 1998 · N995Z · Doug DC932 · Fuselage Miscellaneous Structure
  > MCI - DURING OP 16 MAINTENANCE CHECK, FOUND SUPPORT ANGLE TO FRONT SPAR CRACKED AT BULKHEAD STATION 604, BETWEEN LONGERON 23R AND 24R. REPLACED CRACKED SUPPORT ANGLE, PER SRM 51-01 PAGE 1, ITEM C, AND INSTALLED FASTENERS PER SRM 51-30-2. (M)

Next page: https://openairdocs.org/deregistered/N995Z-2013-03-21/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 = 'N995Z' AND deregistration_id = 'N995Z-2013-03-21'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N995Z-2013-03-21/reports

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