# Service difficulty reports: N498DA, cancelled Dec 10, 2012

A list on [N498DA, cancelled Dec 10, 2012](https://openairdocs.org/deregistered/N498DA-2012-12-10.md).

Matched to this aircraft by N-number and event date, checked against the reported serial number, make and model. Newest first.

- [SDR FOTR2011101406609](https://openairdocs.org/sdr/FOTR2011101406609.md): Frame · corroded · Oct 14, 2011 · N498DA · Boeing 737232 · Fuselage Main, Frame
  > TOP OF FRAME BS 727E, S25L CORRODED. REPAIRED ON FASI WO 21142, NR 06609.
- [SDR FOTR2011100406432](https://openairdocs.org/sdr/FOTR2011100406432.md): Frame · corroded · Oct 4, 2011 · N498DA · Boeing 727232 · Fuselage Main, Frame
  > SURFACE CORROSION AT BS 727, FRAME LBL 5 TO RBL 5, AFT SIDE, LWR AFT CARGO. REPAIRED ON FASI WO 21142, NR 06432.
- [SDR DL72S992769](https://openairdocs.org/sdr/DL72S992769.md): Battery Pack · discharged · Dec 16, 1999 · N498DA · Boeing 727232 · Emergency Lighting
  > ON MTC LAYOVER, LT OUTSIDE EMERGENCY EGRESS LIGHTING INOP. REPLACED FWD LIGHT POWER SUPPLY. REPLACED BULBS FOR MID LIGHT AND REPLACED BATTERY PACK ON AFT LIGHT, OPER NOW NORMAL.
- [SDR DL72S992252](https://openairdocs.org/sdr/DL72S992252.md): Power Supply · failed · Oct 10, 1999 · N498DA · Boeing 727232 · Emergency Lighting
  > CABIN OVERHEAD EMERGENCY LIGHTS INOP ROW 2. REPLACED POWER SUPPLY AND BATTERY PACK.
- [SDR DL72S990904](https://openairdocs.org/sdr/DL72S990904.md): Spar Web · cracked · Apr 24, 1999 · N498DA · Boeing 727232 · Wing Spar
  > WING CENTER SECTION, REAR SPAR WEB, RBL 13. CRACK REPAIR. THE CENTER WING REAR SPAR WEB WAS FOUND WITH A 1.5 INCH LONG TYPICAL CRACK AT RBL 13, JUST BELOW THE UPPER SPAR CAP. THE CRACK WAS ROUTED OUT OF THE SPAR WEB AND REPAIRED WITH AN ALUMINUM DOUBLER PER
- [SDR DL72S990610](https://openairdocs.org/sdr/DL72S990610.md): Skin · cracked · Mar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 681 AND 740 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 19 CRACK INDICATIONS ALONG THE PANEL LENGTH. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE
- [SDR DL72S990609](https://openairdocs.org/sdr/DL72S990609.md): Skin · cracked · Mar 17, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 85 CRACKS INCLUDING A 15 INCH LONG CRACK LINK UP BETWEEN FS 640 AND 660. THE ENTIRE SKI
- [SDR DL72S990608](https://openairdocs.org/sdr/DL72S990608.md): Skin · cracked · Mar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED 8 CRACKS BETWEEN FS 440 AND 460. THE CRACKED AREA OF SKIN LAP SPLICE WAS CUTOUT AND RE
- [SDR DL72S990570](https://openairdocs.org/sdr/DL72S990570.md): Skin · cracked · Mar 16, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4L SKIN LAP SPLICE BETWEEN FS 360 AND 480 INDICATED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN PANEL. INTERNAL HFEC INSPECTION CONFIRMED 2 CRACKS BETWEEN FS 460 AND 480. THE CRACKS WERE ROUTED OUT AND REPAIRED PER B72
- [SDR DL72S990571](https://openairdocs.org/sdr/DL72S990571.md): Skin · cracked · Mar 15, 1999 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 26L SKIN LAP SPLICE BETWEEN FS 481 AND 681 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL HFEC INSPECTION CONFIRMED ONE CRACK BETWEEN FS 580 AND 600. THE CRACK WAS ROUTED OUT AND REPAIRED PER B727 SRM
- [SDR DL72S980807](https://openairdocs.org/sdr/DL72S980807.md): Fitting · cracked · Apr 14, 1998 · N498DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON B2 LETTER CK, LT INBD VERTICAL STAB TIE BOLT FITTING CRACKED 1 INCH AT THE FIRST FASTENER HOLE AFT OF THE TIE BOLT. REPLACED FITTING PER BOEING DRAWING 65-17509.
- [SDR DL72S980806](https://openairdocs.org/sdr/DL72S980806.md): Access Panel · cracked · Apr 14, 1998 · N498DA · Boeing 727232 · Elevator, Plate/Skin
  > FOUND ON B2 LETTER CK, 4 INCH CRACK ON BALANCE BOARD ACCESS PANEL 9114. REPAIRED PER SRM 55-20-3.
- [SDR DL72S971807](https://openairdocs.org/sdr/DL72S971807.md): Valve · failed · Sep 16, 1997 · N498DA · Boeing 727232 · Landing Gear Retraction/Extension System
  > AFTER T/O LOST ALL 'A' HYD SYS QTY AND PRESSURE. REPLACED RT MLG LOCK OPERATED SEQUENCING VALVE.
- [SDR DL72S971782](https://openairdocs.org/sdr/DL72S971782.md): Angle · cracked · Sep 11, 1997 · N498DA · Boeing 727232 · Leading Edge Devices
  > ANGLE AT NR 8 SLAT O/B UPSTOP IS CRACKED. REPAIRED PER M/M 57-54-0 PG 816.
- [SDR DL72S971781](https://openairdocs.org/sdr/DL72S971781.md): Rib · cracked · Sep 11, 1997 · N498DA · Boeing 727232 · Leading Edge Devices
  > NOSE RIB AT NR 7 SLAT IS CRACKED. REPAIRED PER M/M 57-54-0 PG 819. REPAIRED UPPER CRACK PER M/M 57-54-00 PG 809.
- [SDR DL72S971759](https://openairdocs.org/sdr/DL72S971759.md): Skin · cracked · Sep 5, 1997 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > UPON REMOVAL OF A TIME LIMITED REPAIR ON THE UPPER HINGE CUTOUT OF THE R1 DOOR THE CRACK WAS FOUND TO HAVE LENGTHENED TO 2.75 IN THE REINFORCING STRAP/ DOUBLER WHICH IS BEYOND M/M LIMITS. THIS CRACK WAS REPAIRED WITH A DOUBLER PER ERA 362243-14.
- [SDR DL72S972141](https://openairdocs.org/sdr/DL72S972141.md): Skin · cracked · Aug 28, 1997 · N498DA · Boeing 727232 · Trailing Edge Flaps
  > COVE SKIN CRACKED 31 FROM I/B END OF FLAP, REPAIRED PER MM 57-52-0 FIG 809.
- [SDR DL72S971761](https://openairdocs.org/sdr/DL72S971761.md): Flap · cracked · Aug 27, 1997 · N498DA · Boeing 727232 · Trailing Edge Flaps
  > DOUBLER CRACKED AFT SPAR 19 AND 37S FROM I/B END. REPAIRED PER M/M 57-52-0 PG 802.
- [SDR DL72S971645](https://openairdocs.org/sdr/DL72S971645.md): Stringer · cracked · Aug 22, 1997 · N498DA · Boeing 727232 · Wing, Longeron/Stringer
  > OUTER WING UPPER STRINGER TO RIB ATTACHMENT CRACKED AT LT WING STA 629 STR 13. REMOVED FASTENERS, FILLERS, AND WASHERS, CUT ACCESS HOLE PER FIG 803. DRILLED UP REPAIR ANGLE AND RADIUS BLOCKS. REMOVED FASTENERS AT STRINGER 13, 14, 15, DRILLED UP REPAIR AT ST
- [SDR DL72S971949](https://openairdocs.org/sdr/DL72S971949.md): Frame · cracked · Aug 20, 1997 · N498DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME AT STA 910 LT CRACKED INSIDE LT W/W. REPAIRED PER M/M 53-11-0 PG 814.
- [SDR DL72S971948](https://openairdocs.org/sdr/DL72S971948.md): Rib · cracked · Aug 20, 1997 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB CRACKED INBD END NR 5 L/E SLAT. REPAIRED PER M/M 57-54-0 FIG 814.
- [SDR DL72S971695](https://openairdocs.org/sdr/DL72S971695.md): Rib · cracked · Aug 20, 1997 · N498DA · Boeing 727232 · Leading Edge Devices
  > TWO RIBS CRACKED IN NR 6 L/E SLAT. REPAIRED PER M/M 57-54-0 PG 807.
- [SDR DL72S971756](https://openairdocs.org/sdr/DL72S971756.md): Bracket · cracked · Aug 19, 1997 · N498DA · Boeing 727232 · Leading Edge Slat Actuator
  > BRACKETS CRACKED THE NR 5 L/E FLAP I/B ACTUATOR BRACKET HAS PREVIOUS REPAIR STOP DRILL CRACKED BEYOND STOP DRILL. THE O/B NR 5 ACTUATOR BRACKET IS ALSO CRACKED AT LOWER RADIUS. REMOVED ACTUATOR REMOVED O/B BRACKET. STOP DRILLED CRACK. CRACK LENGTH AND REPA
- [SDR DL72S971722](https://openairdocs.org/sdr/DL72S971722.md): Skin · cracked · Aug 18, 1997 · N498DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > R-1 DOOR UPPER HINGE CUTOUT CRACKED. REPAIRED PER ERA362243-14 REV. A.
- [SDR DL72S970418](https://openairdocs.org/sdr/DL72S970418.md): Power Supply · inoperative · Mar 6, 1997 · N498DA · Boeing 727232 · Emergency Lighting
  > AFT SECTION OF TRACK LIGHTING SYS INOP. REPLACED BATTERY PACK AND RACK, CKS OK.
- [SDR DL72S961840](https://openairdocs.org/sdr/DL72S961840.md): Power Supply · inoperative · Aug 3, 1996 · N498DA · Boeing 727232 · Emergency Lighting
  > DURING TEST, CENTER EMERGENCY LIGHTS FLICKER. REPLACED POWER SUPPY, OPS CHECK NORMAL.
- [SDR DL72S961163](https://openairdocs.org/sdr/DL72S961163.md): Web · fatigue · May 15, 1996 · N498DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > THE AFT VENTRAL STAIRWAY TORQUE BOX RT VERTICAL WEB AT STA 1263 HAD A.75 INCH CRACK AT THE NR 2 ENGINE FUEL LINE CUTOUT. MADE SPLICE REPAIR PER ER/A 303593-14.
- [SDR DL72S961154](https://openairdocs.org/sdr/DL72S961154.md): Skin · cracked · May 14, 1996 · N498DA · Boeing 727232 · Nacelle/Pylon, Plate/Skin
  > A 2 INCH CRACK IN NR 2 ENG INLET OUTER SKIN 3 FT FROM INLET LIP, 2 FT UP FROM FUSELAGE SKIN LT SIDE. REPAIRED PER M/M 54-30-0 FIG 801.
- [SDR DL72S961731](https://openairdocs.org/sdr/DL72S961731.md): Rib · cracked · Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 18 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.
- [SDR DL72S961730](https://openairdocs.org/sdr/DL72S961730.md): Rib · cracked · Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 12 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.
- [SDR DL72S961729](https://openairdocs.org/sdr/DL72S961729.md): Rib · cracked · Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 12 WAS CRACKED. INSTALLED REPAIR PER MM 57-54-0 FIG 805.
- [SDR DL72S961727](https://openairdocs.org/sdr/DL72S961727.md): Rib · damaged · Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 11 WAS CRACKED. INSTALLED RIB REPAIR PER MM 57-54-0 FIG 805.
- [SDR DL72S961726](https://openairdocs.org/sdr/DL72S961726.md): Rib · cracked · Apr 16, 1996 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 8 WAS CRACKED. REPAIRED RIB PER MM 57-54-0 FIG 805.
- [SDR DL72S960881](https://openairdocs.org/sdr/DL72S960881.md): Skin · damaged · Apr 12, 1996 · N498DA · Boeing 727232 · Horizontal Stabilizer, Plate/Skin
  > AT MID-VISIT, THE HORIZ STAB PANEL NR 9215 WAS FOUND TO HAVE A HOLE IN THE TOP SURFACE. THE HOLE WAS REPAIRED PER SRM 55-10-2.
- [SDR DL72S960976](https://openairdocs.org/sdr/DL72S960976.md): Blkhd Stiffener · cracked · Apr 8, 1996 · N498DA · Boeing 727232 · Fuselage Main, Bulkhead
  > A CRACK WAS FOUND EMANATING FROM THE BOTTOM OF THE LT FLANGE ON THE VERTICAL STIFFENER FS 1183 AT RBL 8. THE CRACK WAS APPROXIMATELY 0.25 INCH IN LENGTH. S/B 727-53-0175, REV 2, WHICH IS REQUIRED BY A.D. 90-06-09, CONTAINS INSPECTION, MODIFICATION, AND REPAI
- [SDR DL72S960879](https://openairdocs.org/sdr/DL72S960879.md): Doubler · damaged · Apr 5, 1996 · N498DA · Boeing 727232 · Passenger/Crew Doors
  > AT MID-VISIT, A TEMP REPAIR WAS FOUND TO BE INSTALLED ON THE TOP AFT CORNER OF THE L1 DOOR OUTER SKIN. THE DOUBLER WAS REMOVED AND REPAIR INSTALLED PER MM 52-11-01 FIG 804.
- [SDR DL72S960842](https://openairdocs.org/sdr/DL72S960842.md): Frame · cracked · Apr 5, 1996 · N498DA · Boeing 727232 · Service Doors
  > AT MID-VISIT, THE R2 DOOR FRAME WAS FOUND CRACKED JUST BELOW UPPER HINGE CUTOUT. THE DAMAGE WAS ROUTED OUT AND DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.
- [SDR DL72S960841](https://openairdocs.org/sdr/DL72S960841.md): Skin · cracked · Apr 5, 1996 · N498DA · Boeing 727232 · Service Doors
  > AT MID-VISIT, THE R2 DOOR UPPER HINGE ARM CUTOUT WAS FOUND TO BE CRACKED. THE DAMAGE WAS ROUTED OUT AND A DOUBLER PREPARED AND INSTALLED PER SRM 52-40-2.
- [SDR DL72S953990](https://openairdocs.org/sdr/DL72S953990.md): Angle · cracked · Oct 12, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING F-1 LETTER CHECK,.25 INCH CRACK IN RADIUS FROM UNDER BLOCK STA 910 RT MLG UPLOCK H-BRACKET FWD SUPPORT ANGLE. REPAIRED PER M/M 53-11-0 PG 834 AND 835.
- [SDR DL72S953884](https://openairdocs.org/sdr/DL72S953884.md): Frames · misdrilled · Aug 22, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF SI 4-61904-12AD, MAINTENANCE DISCOVERED THAT THE FRAMES AT STA 760.95 LT AND RT AND STA 783.95 LT AND RT HAVE OPEN PILOT HOLES IN THE WEB ABOVE STR 17. THE HOLES WHICH ARE ATTACH POINTS FOR INSULATION BLANKETS, HAVE BEEN INSPECTED AND
- [SDR DL72S951496](https://openairdocs.org/sdr/DL72S951496.md): Rib · cracked · Apr 12, 1995 · N498DA · Boeing 727232 · Leading Edge Devices
  > DURING SHOP, INSPECTION RT WING NR 5 L/E SLAT WAS FOUNED WITH RIB NR 12 CRACKED. REPAIRED PER MM 57-54-00.
- [SDR DL72S951407](https://openairdocs.org/sdr/DL72S951407.md): Rib · cracked · Apr 4, 1995 · N498DA · Boeing 727232 · Leading Edge Devices
  > RIB NR 18 CRACKED NEXT TO NUTPLATE. INSTALLED DOUBLER PER MM 57-54-0 FIGURE 805. DURING SHOP INSPECTION OF RT WING NR 5 L/E SLAT.
- [SDR DL72S951335](https://openairdocs.org/sdr/DL72S951335.md): Web · cracked · Mar 30, 1995 · N498DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > VERT WEB CRACKED.625 INCH AT UPPER FASTENER ROW STA 1273, 48 SEC TORQUE BOX. FOUND AT E-2 LTR CK.
- [SDR DL72S951334](https://openairdocs.org/sdr/DL72S951334.md): Skin · cracked · Mar 30, 1995 · N498DA · Boeing 727232 · Vertical Stabilizer, Plate/Skin
  > A 1.25 INCH CRACK IN VERT STAB SKIN RT SIDE AT CUTOUT FOR PANEL 9501 SADDLE PLATE. FOUND DURING E-2 LR CK. REPAIRED PER SRM 55-30-3 PAMM.

## 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 = 'N498DA' AND deregistration_id = 'N498DA-2012-12-10'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N498DA-2012-12-10/reports

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