# Service difficulty reports: N419DA, cancelled Nov 7, 2012

A list on [N419DA, cancelled Nov 7, 2012](https://openairdocs.org/deregistered/N419DA-2012-11-07.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 · 57 reports

- [SDR DL72S001005](https://openairdocs.org/sdr/DL72S001005.md): Frame · cracked · May 22, 2000 · N419DA · Boeing 727232 · Fuselage Main, Structure
  > FOUND ON A1 LETTER CHECK, 1 INCH CRACK R-1 DOOR AFT FRAME AT LOWER STOP CASTING. REPAIRED PER MM 52-12-0.
- [SDR DL72S000795](https://openairdocs.org/sdr/DL72S000795.md): Rib · cracked · Mar 7, 2000 · N419DA · Boeing 727232 · Leading Edge Devices
  > NR 3 SLAT RIB NR 6 CRACKED. INSTALLED DOUBLER PER MM 57-54-00 PG 818.
- [SDR DL72S992660](https://openairdocs.org/sdr/DL72S992660.md): Bulb · failed · Dec 6, 1999 · N419DA · Boeing 727232 · Emergency Lighting
  > ON SVC CHECK, FOUND RT R1 EMERGENCY LIGHT INOP. REPLACED BULB, OPS CK GOOD.
- [SDR DL72S992323](https://openairdocs.org/sdr/DL72S992323.md): Stringer · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STRINGER 18A CRACKED AT LWR AFT BOLT STA 940. REPAIRED PER MM 53-12-0 PG 816.
- [SDR DL72S992322](https://openairdocs.org/sdr/DL72S992322.md): Bracket · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Leading Edge Slat Actuator
  > NR 1 SLAT ACTUATOR O/B MOUNT BRACKET CRACKED ON WEB. REPAIRED PER M/M 57-20-21 PG 812.
- [SDR DL72S992321](https://openairdocs.org/sdr/DL72S992321.md): Skin · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > TWO.25 INCH CRACKS IN F/S 231 STR 21R. INSTALLED DOUBLER PER SRM 53-30-3 F 26.
- [SDR DL72S992320](https://openairdocs.org/sdr/DL72S992320.md): Web · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TPA LTR CHECK F-2, LT TORQUE BOX VERT WEB CRACKED 1 AT STA 1235. REPAIRED PER MM 53-11-0.
- [SDR DL72S992319](https://openairdocs.org/sdr/DL72S992319.md): Skin · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Horizontal Stabilizer, Plate/Skin
  > TPA LTR CHECK F-2, 1 CRACK IN VERT STAB SKIN LT SIDE AT LWR SIDE OF CUTOUT FOR ACCESS PANEL 9523. REPAIRED PER MM 54-30-0.
- [SDR DL72S992317](https://openairdocs.org/sdr/DL72S992317.md): Frame · cracked · Oct 21, 1999 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND AT F-2 LTR CK, AFT ENTRY DOOR FRAME CUTOUT CRACKED LT SIDE BELOW A/C DATA PLATE. REPAIRED PER SRM 53-10-9.
- [SDR DL72S991866](https://openairdocs.org/sdr/DL72S991866.md): Prbc · inop · Aug 20, 1999 · N419DA · Boeing 727232 · Compressor Bleed Valve
  > AUTO PACK TRIP ON TAKEOFF. POSSIBLE COMPRESS STALL. OCCURED AFTER BRAKES RELEASE. ABORTED TAKEOFF AT 60 KTS. REPLACED NR 3 ENGINE PRBC FOR OFF IDLE STALL. RAN ENG PER PHHB, ALL INDICATIONS CKS OK. NO STALLS.
- [SDR DL72S990510](https://openairdocs.org/sdr/DL72S990510.md): Angle · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge Devices
  > REPAIR ANGLE CRACKED NR 7 SLAT STOP PAD I/B SIDE. REPAIRED PER MM 57-54-0 PG 816.
- [SDR DL72S990509](https://openairdocs.org/sdr/DL72S990509.md): Skin · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > A.25 INCH CRACK FUSELAGE SKIN AT FASTENER JUST AFT OF L-3 COCKPIT WINDOW. REPAIRED PER SRM 53-30-3 FIG 8.
- [SDR DL72S990508](https://openairdocs.org/sdr/DL72S990508.md): Bracket · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge Slat Actuator
  > FOUND ON F1 LETTER CK, CRACK IN NR 1 SLAT ACTUATOR SUPPORT BRACKET WEB I/B SIDE. REPAIRED PER MM 57-20-21.
- [SDR DL72S990507](https://openairdocs.org/sdr/DL72S990507.md): Stiffener · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON F1 LETTER CK, L/E SPAR STIFFENER CRACKED AT LOWER END NR 3 SLAT O/B TRACK I/B SIDE. REPAIRED PER MM 57-20-21.
- [SDR DL72S990505](https://openairdocs.org/sdr/DL72S990505.md): Skin · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Elevator, Plate/Skin
  > A.5 INCH CRACK IN RT ELEVATOR LOWER SKIN AT FWD SPAR AREA. REPAIRED PER SRM 55-20-3 FIG 4.
- [SDR DL72S990501](https://openairdocs.org/sdr/DL72S990501.md): Frame · cracked · Mar 10, 1999 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON F1 LETTER CK, AFT ENTRY DOOR FRAME CRACKED RT SIDE 10 INCHES BELOW THE TOP OF THE DOOR CUTOUT. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990313](https://openairdocs.org/sdr/DL72S990313.md): Battery Pack · discharged · Feb 16, 1999 · N419DA · Boeing 727232 · Emergency Lighting
  > OVERHEAD EXIT SIGN EMERGENCY LIGHT INOP ON TEST AT OVERWING EXITS. REPLACED M1094 RACK AND BATTERY PACK OP CKS OK. PARTS BORROWED FROM AMERICA WEST PACK LOCATED ABOVE ROW 19 RT SIDE OF CTR DUCT.
- [SDR DL72S990312](https://openairdocs.org/sdr/DL72S990312.md): Battery Pack · discharged · Feb 16, 1999 · N419DA · Boeing 727232 · Emergency Lighting
  > LEFT EXTERIOR OVERWING EMERGENCY EXIT LIGHT MOST FWD INOP. REPLACED RACK AND BATTERY PACK, OP CKS OK.
- [SDR DL72S982360](https://openairdocs.org/sdr/DL72S982360.md): Light · inop · Nov 14, 1998 · N419DA · Boeing 727232 · Emergency Lighting
  > L2 DOOR EMERG EXIT LIGHT INOP. REPLACED LIGHT ASSY.
- [SDR DL72S981594](https://openairdocs.org/sdr/DL72S981594.md): Skin · dented · Jul 31, 1998 · N419DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > THE FUSELAGE SKIN WAS BADLY DENTED AT FS 295 BETWEEN STR 12L AND 13L DUE TO A BIRD STRIKE. THE DAMAGED AREA WAS CUTOUT AND REPAIRED PER THE B727 SRM 53-30-3, FIG 1 WITH AN EXTERNAL ALUMINUM REPAIR DOUBLER. THE REPAIR WAS DOCUMENTED PER ER/A 365361-14 WHICH A
- [SDR DL72S980102](https://openairdocs.org/sdr/DL72S980102.md): Web · cracked · Jan 14, 1998 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSTALLATION OF PREVENTATIVE MOD ON THE LHS KEEL BEAM PER SB727-53-0208 (EO 4-64433-3), A CRACK WAS FOUND IN THE WEB JUST ABOVE THE VERT FLANGE OF THE KEEL BEAM. REPAIRED PER ERA 331201-14.
- [SDR DL72S980101](https://openairdocs.org/sdr/DL72S980101.md): Skin · cracked · Jan 14, 1998 · N419DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > DURING INSPECTION PER EO4-60829-3, A CRACK WAS FOUND IN THE SKIN AND DOUBLER IN THE TYP LOCATION AS WELL AS A CRACK IN THE STRAP, BUT ONE FASTENER ROW HIGHER THAN TYP. REPAIRED PER ERA 331195-14.
- [SDR DL72S980063](https://openairdocs.org/sdr/DL72S980063.md): Skin · cracked · Jan 7, 1998 · N419DA · Boeing 727232 · Leading Edge Devices
  > NUMBER 4 L/E SLAT HAD A CRACK FROM THE FENCE MOUNTING BOLT HOLE. INSTALLED A REPAIR DOUBLER PER M/M 57-54-0.
- [SDR DL72S971808](https://openairdocs.org/sdr/DL72S971808.md): Light · damaged · Sep 16, 1997 · N419DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY TRACK LIGHTING STRIP AT 22DEF, TRACK COVER AND WIRING DAMAGED. REPLACED APPROX 30 INCHES OF LIGHT TRACK INVOLVING 4 RED LIGHTS. REPLACING 1 BULB HOLDER REPAIRED DAMAGED WIRING. INSTALLED 4 NEW RED LENS.
- [SDR DL72S970245](https://openairdocs.org/sdr/DL72S970245.md): Battery Pack · discharged · Feb 8, 1997 · N419DA · Boeing 727232 · Emergency Lighting
  > RT CARGO DOOR EMERGENCY LIGHT INOP. REPLACED BATTERY PACK AT M957, OPS CHKS GOOD.
- [SDR DL72S970071](https://openairdocs.org/sdr/DL72S970071.md): Battery · discharged · Jan 15, 1997 · N419DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY EXIT LIGHT OUT AT ROW 16. REPLACED BATTERY AND RACK.
- [SDR DL72S962440](https://openairdocs.org/sdr/DL72S962440.md): Battery · discharged · Nov 3, 1996 · N419DA · Boeing 727232 · Emergency Lighting
  > EMERGENCY LIGHT ABOVE L1 DOOR INOP. REPLACED BATTERIES.
- [SDR DL72S962414](https://openairdocs.org/sdr/DL72S962414.md): Web · cracked · Oct 29, 1996 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > A.75 INCH CRACK AT LIGHTNING HOLE STATION 1243 LT, LOWER TORQUE BOX WEB. INSTALLED DOUBLER PER MM 53-11-0 PG 828.
- [SDR DL72S962025](https://openairdocs.org/sdr/DL72S962025.md): Battery Pack · discharged · Sep 1, 1996 · N419DA · Boeing 727232 · Emergency Lighting
  > OVERWING EXIT LIGHT AT AFT CARGO DOOR INOP. REPLACED BATTERY CARTRIDGE, OPS CHECK GOOD.
- [SDR DL72S960754](https://openairdocs.org/sdr/DL72S960754.md): Stringer · cracked · Apr 2, 1996 · N419DA · Boeing 727232 · Vertical Stabilizer
  > FOUND ON C-2 LETTER CHECK, VERT STAB STRINGER CRACKED RT SIDE TAIL CRAWLWAY, FOURTH BAY UP. REPAIRED PER M/M 53-30-0.
- [SDR DL72S960753](https://openairdocs.org/sdr/DL72S960753.md): Angle · cracked · Apr 2, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > FOUND ON C-2 LETTER CHECK, NR 1 SLAT COVE SKIN ATTACH ANGLE CRACKED BELOW THE ANTI-ICE DUCT. REPAIRED PER M/M 57-54-0.
- [SDR DL72S960555](https://openairdocs.org/sdr/DL72S960555.md): Rib · cracked · Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > THE I/B ACTUATOR RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.
- [SDR DL72S960554](https://openairdocs.org/sdr/DL72S960554.md): Rib · cracked · Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > THE NR 9 RIB WAS FOUND TO BE CRACKED. REPAIRED PER M/M 57-54-0 FIG 804, FOR NR 6 L/E SLAT PANEL.
- [SDR DL72S960553](https://openairdocs.org/sdr/DL72S960553.md): Rib · cracked · Feb 29, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > THE O/B ACTUATOR RIB WAS FOUND TO BE CRACKED IN 2 PLACES. REPAIRED PER M/M 57-54-0 FIGS 804 AND 814, FOR NR 6 L/E SLAT PANEL.
- [SDR DL72S960389](https://openairdocs.org/sdr/DL72S960389.md): Rib · cracked · Feb 20, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION, NR 4 L/E SLAT WAS FOUND WITH FOUR CRACKED/DAMAGED LEADING EDGE SUPPORT RIBS. REPAIRED PER MM 57-54-0.
- [SDR DL72S960385](https://openairdocs.org/sdr/DL72S960385.md): Skin · cracked · Feb 20, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION, NR 4 L/E SLAT OUTER SKIN WAS FOUND CRACKED AT FENCE ATTACH MOUNT HOLE. REPAIRED SKIN PER MM 57-54-0 FIG 813.
- [SDR DL72S960463](https://openairdocs.org/sdr/DL72S960463.md): Rib · cracked · Jan 29, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > DURING INSPECTION, NR 6 L/E SLAT WAS FOUND WITH NR 1 L/E SUPPORT RIB CRACKED. REPAIRED PER MM 57-54-0.
- [SDR DL72S961604](https://openairdocs.org/sdr/DL72S961604.md): Frame · corrosion · Jan 20, 1996 · N419DA · Boeing 727232 · Fuselage Main, Frame
  > THE BS 1166 FRAME WAS FOUND CORRODED NEAR STRINGER 29R. THE REMOVED SECTION OF FRAME WAS TOO LARGE TO REPAIR PER THE B727 SRM. THE FRAME WEB IS MANUFACTURED FROM 0.063 CLAD 7075-T6. ALSO, THERE IS A FACTORY INSTALLED 0.050 CLAD 7075-T6 BONDED DOUBLER INSTAL
- [SDR DL72S960170](https://openairdocs.org/sdr/DL72S960170.md): Keel Beam · corroded · Jan 19, 1996 · N419DA · Boeing 727232 · Fuselage Main, Keel
  > DURING INSPECTION, THE OUTBD FLANGE OF THE RT KEEL BEAM, STR 29R WAS FOUND WITH CORROSION AT STA 950. DUE TO INTERFERENCE ITEMS IT WAS NECESSARY TO CUT THE FUSELAGE SKIN TO REMOVE THE CORRODED FLANGE. REPAIR DOUBLERS AND STRAPS WERE INSTALLED IN ACCORDANCE W
- [SDR DL72S960169](https://openairdocs.org/sdr/DL72S960169.md): Stringer · cracked · Jan 19, 1996 · N419DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > DURING INSPECTION, CORROSION WAS REMOVED BY BLENDING AND SPOT FACING IN SEVERAL LOCATIONS ON THE UPPER SURFACE OF THE O/B AND I/B SKIN FLANGES, STRINGER 29L BETWEEN STA 950 AND STA 970. MINIMUM REMAINING FLANGE THICKNESS WAS.100. ALL CORROSION BLENDS ARE CO
- [SDR DL72S960129](https://openairdocs.org/sdr/DL72S960129.md): Floor Pan · cracked · Jan 11, 1996 · N419DA · Boeing 727232 · Fuselage Floor Panel
  > FOUND ON MV1 CHECK, LT AND RT LAV FLOOR PAN DITCHING SEAL PANEL CRACKED, VIEWED FROM BAG BIN FWD OF 1183. REPAIRED PER M/M 53-0-11.
- [SDR DL72S960475](https://openairdocs.org/sdr/DL72S960475.md): Rib · cracked · Jan 9, 1996 · N419DA · Boeing 727232 · Leading Edge Devices
  > UPON ROUTINE INSPECTION, A CRACK WAS FOUND ON 2ND RIB FROM I/B END. REPAIRED AS PER SRM 57-50-3 FIG 9, FOR NR L/E SLAT.
- [SDR DL72S954273](https://openairdocs.org/sdr/DL72S954273.md): Battery · discharged · Nov 7, 1995 · N419DA · Boeing 727232 · Emergency Lighting
  > AFT AIRSTAIR EMERGENCY LIGHT INOP. REPLACED BATTERY, CHECKS NORMAL.
- [SDR DL72S953685](https://openairdocs.org/sdr/DL72S953685.md): Battery Pack · discharged · Sep 12, 1995 · N419DA · Boeing 727232 · Emergency Lighting
  > LT AND RT LOWER OVERWING EXTERIOR EMERGENCY LIGHTS INOP. REPLACED BATTERY PACKS EACH SIDE. RT SIDE CKS NORMAL. LT SIDE FORWARD TO MCO.
- [SDR DL72S953643](https://openairdocs.org/sdr/DL72S953643.md): Rib · cracked · Sep 6, 1995 · N419DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP INSPECTION, THE 4TH RIB FOR I/B END WAS FOUND CRACKED. THE RIB WAS REPAIRED PER SRM 57-54-00. THE LOWER COVE PANEL ATTACH ANGLE UNDERNEATH THE I/B UPSTOP WAS FOUND TO HAVE A CRACK. THE ANGLE WAS REPAIRED PER SRM 57-54-0 FIG 812, FOR NR 2 L/E SLA
- [SDR DL72S953549](https://openairdocs.org/sdr/DL72S953549.md): Beam · cracked · Aug 29, 1995 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > AT A LETTER CHECK IN TPA, A.50 INCH CRACK WAS FOUND IN THE UPPER TRANSVERSE BEAM GUSSET ANGLE AT F.S. 1273. ALSO, A.75 INCH CRACK IN THE ACCOMPANYING UPPER TRANSVERSE BEAM AT F.S. 1273. THE DAMAGED PARTS WILL BE REPLACED IN ACCORDANCE WITH B727 S/B 53-0129
- [SDR DL72S953531](https://openairdocs.org/sdr/DL72S953531.md): Angle · cracked · Aug 28, 1995 · N419DA · Boeing 727232 · Leading Edge Devices
  > CRACK, 25 INCHES, NR 2 SLAT INBOARD UPSTOP PAD. FOUND AT C-1 LTR CK. SLAT WAS REPLACED AND ROUTED TO SHOP.
- [SDR DL72S953530](https://openairdocs.org/sdr/DL72S953530.md): Rib · cracked · Aug 28, 1995 · N419DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT HAS.50 INCH CRACK INBOARD OF ACTUATOR ATTACH POINT AT FORWARD RIB. FOUND AT C-1 LTR CK. REPAIRED PER MM 57-54-0.
- [SDR DL72S951452](https://openairdocs.org/sdr/DL72S951452.md): Actuator · cracked · Apr 7, 1995 · N419DA · Boeing 727232 · Leading Edge Slat Actuator
  > ON APPROACH, LOST SYSTEM A HYDRAULICS. LANDED ATL AND FOUND NR 7 SLAT ACTUATOR CRACKED. REPLACED ACTUATOR, OPERATION NORMAL.
- [SDR DL72S950813](https://openairdocs.org/sdr/DL72S950813.md): Angle · cracked · Feb 16, 1995 · N419DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING INSPECTION, THE RT TORQUE BOX UPPER TRANSVERSE BEAM GUSSET ANGLE AT FS 1273 WAS FOUND CRACKED. THE ANGLE WAS REPLACED IN ACCORDANCE WITH B727 SB 53-0129 REV 4.

Next page: https://openairdocs.org/deregistered/N419DA-2012-11-07/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 = 'N419DA' AND deregistration_id = 'N419DA-2012-11-07'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N419DA-2012-11-07/reports

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