# Service difficulty reports: N403DA, cancelled Aug 15, 2013

A list on [N403DA, cancelled Aug 15, 2013](https://openairdocs.org/deregistered/N403DA-2013-08-15.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 · 65 reports

- [SDR DL72S001117](https://openairdocs.org/sdr/DL72S001117.md): Actuator · failed · Jun 8, 2000 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > DURING FLIGHT BETWEEN DFW AND SEA AT FLT LEVEL 310, CREW EXPERIENCED AN A-SYSTEM LOW HYDRAULIC PRESSURE LIGHT FLICKERING. CREW THEN NOTICED THE A-SYSTEM QUANTITY INDICATION WAS AT ZERO. DIVERTED TO SLC. WHEN LOWERING FLAPS WITH ALTERNATE SYSTEM, CREW COULD
- [SDR DL72S000905](https://openairdocs.org/sdr/DL72S000905.md): Skin · cracked · May 4, 2000 · N403DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 & 480 INDICATED A CRACK IN THE LOWER FASTENER ROW OF THE LOWER SKIN. INTERNAL MFEC INSPECTION ALONG THE LENGTH OF THE PANEL CONFIRMED A SINGLE CRACK LOCATION BETWEEN FS 360 & 380. THE CRACK WA
- [SDR DL72S000555](https://openairdocs.org/sdr/DL72S000555.md): Actuator · leaking · Mar 21, 2000 · N403DA · Boeing 727232 · Leading Edge Slat Control System
  > LOST A SYSTEM HYD QTY DURING CLIMBOUT. FOUND NUMBER 6 LEADING EDGE FLAP ACTUATOR LEAKING. REPLACED NR 6 LEADING EDGE FLAP ACTUATOR AND A SYS CASE DRAIN AND PRESS FILTERS.
- [SDR DL72S000537](https://openairdocs.org/sdr/DL72S000537.md): Bulb · failed · Mar 20, 2000 · N403DA · Boeing 727232 · Emergency Lighting
  > AFT LT OVERWING EMERGENCY LIGHT INOP. FOUND SEVERAL BULBS INOP. REPLACED BAD BULBS AFT LT OVERWING EMER EXIT SIGN, NOW CHECKS OK. ONLY BULBS INOP WERE ONES THAT LIGHT SIGN AT ALL TIMES.
- [SDR DL72S992601](https://openairdocs.org/sdr/DL72S992601.md): Oven · contaminated · Nov 25, 1999 · N403DA · Boeing 727232 · Buffet/Galleys
  > FORWARD GALLEY WORK LIGHT C/B POPPED. F/A REPORTED LIGHT PLASTIC SMELL. NO SMOKE NOTED. BREAKER WAS NOT RESET. ON CHECK, FOUND GALLEY WORK LIGHT C/B POPPED AND COLLARED BY PREVIOUS ENG ORDER. CHKD OPS OF OVENS, COFFEEMAKER. ALL ELEC OPERATIONS NORMAL. FO
- [SDR DL72S992429](https://openairdocs.org/sdr/DL72S992429.md): Bracket · cracked · Nov 2, 1999 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > A.125 INCH CRACK IN NR 2 L/E FLAP ACTUATOR SUPPORT BOX INBD LWR BRACKET. INSTALLED DOUBLER PER M/M 57-20-21.
- [SDR DL72S992428](https://openairdocs.org/sdr/DL72S992428.md): Frame · cracked · Nov 2, 1999 · N403DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C2 LETTER CHECK, 1.5 INCH CRACK ON R-1 DOOR FWD FRAME AT THE LOWER STOP CASTING. REPAIRED PER ERA AND MM 52-12-0.
- [SDR DL72S990716](https://openairdocs.org/sdr/DL72S990716.md): Frame · cracked · Mar 31, 1999 · N403DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND ON C1 LETTER CK, AFT RT ENTRY DOOR FRAME CRACKED. REPAIRED PER SRM 53-10-9.
- [SDR DL72S990560](https://openairdocs.org/sdr/DL72S990560.md): Skin · cracked · Mar 10, 1999 · N403DA · 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. HFEC INTERNAL INSPECTION CONFIREMD SEVERAL CRACKS. THE SKIN LAP SPLICE WAS CUT OUT ALONG THE ENTIRE LENGTH OF THE PA
- [SDR DL72S990549](https://openairdocs.org/sdr/DL72S990549.md): Skin · cracked · Mar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 481 AND 681 REVEALED A CRACK BETWEEN FS 660 AND 681 IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE PANEL CONFIRMED THE SINGLE CRACK. THE CRACK WAS ROUTED OUT O
- [SDR DL72S990548](https://openairdocs.org/sdr/DL72S990548.md): Skin · cracked · Mar 9, 1999 · N403DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > LFEC INSPECTION OF THE STRINGER 4R SKIN LAP SPLICE BETWEEN FS 360 AND 480 REVEALED CRACKS IN THE LOWER FASTENER ROW OF THE LOWER SKIN. HFEC INTERNAL INSPECTION OF THE ENTIRE SKIN PANEL CONFIRMED ONE CRACK BETWEEN FS 400 AND 420. THE CRACK AREA WAS ROUTED OUT
- [SDR DL72S990356](https://openairdocs.org/sdr/DL72S990356.md): Light · inop · Feb 22, 1999 · N403DA · Boeing 727232 · Emergency Lighting
  > ON LAYOVER CK, FOUND R-1 DOOR OVERHEAD EMERGENCY LIGHT INOP. REPLACED LIGHT ASSY PER M/M, CKS OK.
- [SDR DL72S982389](https://openairdocs.org/sdr/DL72S982389.md): Actuator · failed · Nov 18, 1998 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > A-SYS HYD FAILURE ON APPROACH. FOUND THE NR 4 L/E SLAT ACT FAILED. REPLACED SAME.
- [SDR DL72S981781](https://openairdocs.org/sdr/DL72S981781.md): Bulkhead Web · cracked · Aug 26, 1998 · N403DA · Boeing 727232 · Fuselage Main, Bulkhead
  > TWO CRACKS OF.75 INCH LENGTH OR LESS WERE FOUND IN THE FS 1183 BULKHEAD WEB AT RBL 18 BETWEEN WL 166 AND 169 AND ONE.375 INCH CRACK WAS FOUND IN THE WEB AT LBL 25, WL 169. THE CRACKS WERE REPAIRED WITH A DOUBLER PER ER/A 365537-14 AND SET UP FOR REPETITIVE
- [SDR DL72S981620](https://openairdocs.org/sdr/DL72S981620.md): Angle · cracked · Jun 26, 1998 · N403DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER CHORD ANGLE WAS FOUND CRACKED IN 21 PLACES AT I/B CUTOUT FOR I/B AFT FLAP DRIVE. THE ANGLE WAS REPAIRED BY STOP DRILLING THE CRACKS AND INSTALLING A DOUBLER PER 727 MM 57-52-0, PG 807.
- [SDR DL72S981183](https://openairdocs.org/sdr/DL72S981183.md): Actuactor · leaking · Jun 3, 1998 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > IN CRUISE FLIGHT LEVEL 310 A SYSTEM QTY RAPIDLY DECREASED TO ZERO FOLLOWED BY A SYSTEM PRESSURE DECREASING TO ZERO. WHILE RUNNING POM OUTBOARD FLAPS FAILED TO ALT EXTEND. REPLACED NR 3 LED FLAP ACUTATOR. REPLACED NR 1 AND NR 2 HYD CASE DRAIN FILTERS. LEAK
- [SDR DL72S980406](https://openairdocs.org/sdr/DL72S980406.md): Rib · cracked · Feb 19, 1998 · N403DA · Boeing 727232 · Leading Edge Devices
  > NR 6 SLAT RIB CRACKED. REPAIRED PER M/M 57-54-0.
- [SDR DL72S980243](https://openairdocs.org/sdr/DL72S980243.md): Fitting · mislocated · Jan 29, 1998 · N403DA · Boeing 727232 · Wing Miscellaneous Structure
  > WHILE PERFORMING A REPAIR TO WING STR 9 PER MM 57-13-0, FIG 802 AT WS656.5 AN EXISTING HOLE ON THE TOP FLANGE OF THE RIB CHORD ASSY FALLS OUT IN THE RADIUS OF THE STRINGER TO RIB ATTACHMENT ANGLE. REWORKED PER ERA 331251-14AD.
- [SDR DL72S980220](https://openairdocs.org/sdr/DL72S980220.md): Frame · cracked · Jan 26, 1998 · N403DA · Boeing 727232 · Fuselage Main, Frame
  > THE 65C20303-13 REPLACEMENT WEB PREVIOUSLY INSTALLED AS PART OF THE 65C20303-25 FRAME REPAIR KIT WAS FOUND CRACKED. THE -25 KIT WAS INSTALLED BY ERA 111762-14, CIRCA 6/86. THE CRACK IS LOCATED AT APPROX WL216. REPAIRED PER ERA 331194-14AD.
- [SDR DL72S980204](https://openairdocs.org/sdr/DL72S980204.md): Skin · damaged · Jan 23, 1998 · N403DA · Boeing 727232 · Fuselage Main, Plate/Skin
  > FUSELAGE SKIN DAMAGE AT BS 1030 AND S3L OCCURRED. REPAIRED PER ERA 331249-14.
- [SDR DL72S980147](https://openairdocs.org/sdr/DL72S980147.md): Stringer · corroded · Jan 19, 1998 · N403DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STRINGER 30 WAS CORRODED NEAR FS 990. THE STRINGER WILL BE CUT AT FS 990 AND A REPLACEMENT SECTION SPLICED IN. REPAIR PER ERA331185-14.
- [SDR DL72S980403](https://openairdocs.org/sdr/DL72S980403.md): Skin · cracked · Dec 31, 1997 · N403DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP INSPECTION, THE AFT LOWER SPAR ANGLE WAS FOUND CRACKED. THE ANGLE WAS REPAIRED PER 727 MM 57-52-0 BY INSTALLING A REPAIR ANGLE.
- [SDR DL72S980120](https://openairdocs.org/sdr/DL72S980120.md): Angle · damaged · Dec 27, 1997 · N403DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > TEMPORARY REPAIR STA 1343 BL 0 AFT AIRSTAIR OPENING AFT EDGE LWR SIDE. REMOVED REPAIR, CHORD ANGLE, NR 2 ENG FIREWALL PNL. BEGAN DRILLED NEW CHORD AND SKIN. COMPLETED DRILLING CHORD. OK TO INST CHORD. BEGAN INSTALLING CHORD. FINISHED INSTALLING CHORD. C
- [SDR DL72S980189](https://openairdocs.org/sdr/DL72S980189.md): Skin · worn · Dec 23, 1997 · N403DA · Boeing 727232 · Trailing Edge Flaps
  > DURING SHOP VISIT INSPECTION, THE MIDFLAP LEADING EDGE WAS FOUND WORN BEYOND SRM LIMITS AT THE IB END OF FLAP. THE LEADING EDGE WAS REPAIRED PER 727 MM 57-52-0 BY REMOVING THE DAMAGE AND INSTALLING A DOUBLER.
- [SDR DL72S980168](https://openairdocs.org/sdr/DL72S980168.md): Rib · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Rib/Bulkhead
  > ITEM: AT HMV2 FOUND R/W STA 656-5 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC 2ND STRINGER FWD OF REAR SPAR. PLUGGED HOLE PER ERA 33125-14AD STOP DRILLED/REPAIR PART PER MM 57-13-0 FABD PART PER ERA.
- [SDR DL72S980109](https://openairdocs.org/sdr/DL72S980109.md): Web · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Leading Edge Devices
  > NR 6 L/E SLAT INTERNAL WEB CRACKED ON O/B SIDE OF SLAT TRACK MT FITTING. REPAIRED PER MM 57-40-00.
- [SDR DL72S980054](https://openairdocs.org/sdr/DL72S980054.md): Stringer · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/Stringer
  > ITEM: LH WING HFEC INSP SHOWS CRACK INDICATION AT UPPER STRINGER-TO-RIB NO. 8 AT W.S. 546.5. CORRECTION: COMPLETED STEPS #1 THRU 4 PER MM 57-13-0 FIG 802. FINISHED DRILLING REPAIR ANGLES PER MM 57-13-0 FIG 802. OK TO INSTALL. BEGAN INSTALLING REPAIR PER MM 57
- [SDR DL72S980052](https://openairdocs.org/sdr/DL72S980052.md): Stringer · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/Stringer
  > RIGHT WING STA 656.6 UPPER STRINGER TO RIB ATTACH IS CRACKED LOC AT FWD VENT BOX AFT LUG. PROVIDED CUTOUT IN VENT STRINGER FOR ACCESS AS PER DETAIL I M/M 57-13-0 PG 806. FORWARD ANGLE IN PLACE, NEED TO DRILL UP TO VENT BOX STRINGER. DRILLED UP FWD AND REPA
- [SDR DL72S980051](https://openairdocs.org/sdr/DL72S980051.md): Stringer · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/Stringer
  > RT WING HFEC INSP SHOWS CRACK INDICATION AT NO 13 STRINGER-TO-RIB HOLE AT WS 629.0. DRILLED ACCESS HOLE PER M/M 57-13-0. DRILLED REPAIR PARTS PER M/M 57-13-0. OK TO INSTALL. INSTALLED REPAIR PER M/M 57-13-0.
- [SDR DL72S980030](https://openairdocs.org/sdr/DL72S980030.md): Stringer · cracked · Dec 23, 1997 · N403DA · Boeing 727232 · Wing, Longeron/Stringer
  > LEFT WING STA 601.5 UPPER STRINGER TO RIB ATTACH IS CRACKED. FIRST STRINGER FWD OF REAR SPAR. REPAIRED PER MM 57-13-0.
- [SDR DL72S980108](https://openairdocs.org/sdr/DL72S980108.md): Web · cracked · Dec 22, 1997 · N403DA · Boeing 727232 · Vertical Stabilizer
  > WEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED LT SIDE OF VERTICAL, APPROX STA 1303 ABOVE S-DUCT. REPAIRED PER SRM 53-10-4.
- [SDR DL72S980107](https://openairdocs.org/sdr/DL72S980107.md): Web · cracked · Dec 22, 1997 · N403DA · Boeing 727232 · Vertical Stabilizer
  > WEB CRACKED VERTICAL STAB INTERIOR, WEB CRACKED RT SIDE OF VERTICAL APPROX STA 1303. REPAIRED PER SRM 53-10-4.
- [SDR DL72S980053](https://openairdocs.org/sdr/DL72S980053.md): Frame · cracked · Dec 22, 1997 · N403DA · Boeing 727232 · Fuselage Main, Frame
  > STA 930 FRAME AT STR 14 FRAME CRACK AND VERTICAL SKIN STRAP CRACK AT SAME LOCATION. REMOVED FASTENERS AND CUT OUT REPAIR AREA PER SRM 53-10-4 PG 7. ALSO, PERFORMED DYE PENETRANT CHECK PER PS 900-6-3 NR 1. DYE CHECK OK. BEGAN DRILLING REPAIR ANGLES, FINISH
- [SDR DL72S980050](https://openairdocs.org/sdr/DL72S980050.md): Web · cracked · Dec 22, 1997 · N403DA · Boeing 727232 · Leading Edge Devices
  > WEB CRACKED NR 1 SLAT ACTUATOR ATTACH HOUSING WEBS BOTH CRACKED I/B AND O/B SIDE. FABRICATED AND DRILLED I/B REPAIR PER M/M 57-54-0 FIG 804. FABRICATED AND DRILLED UP O/B REPAIR AS PER M/M 57-40-0 FIG 804. OK TO INSTALL. INSTALLED REPAIRS PER M/M 57-54-0
- [SDR DL72S980029](https://openairdocs.org/sdr/DL72S980029.md): Skin · cracked · Dec 22, 1997 · N403DA · Boeing 727232 · Nacelle/Pylon Structure
  > S-DUCT INTERIOR SKIN CRACKED AND BENT UPWARD FROM 10 O'CLOCK TO 1 O'CLOCK POSITION. REMOVED DAMAGED SECTION OF SKIN. FAB REPAIR DOUBLER AND FILLER PER ERA 331180-14. INSTALLED DOUBLER PER ERA 331180. INSTALLED TAPERED SHIM AND CLOSED OUTER SKIN PER ERA 331
- [SDR DL72S980056](https://openairdocs.org/sdr/DL72S980056.md): Stringer · cracked · Dec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, Longeron/Stringer
  > STR 18L, INDICATIONS FOUND 3 EA ON TOP ROW, 2ND HOLE FROM FRONT. ON BOTTOM ROW 1ST AND 3RD HOLE FROM FRONT. REFERENCE SUPPLEMENTAL CARD - ATTACHMENT A OPN 250. CLEANED HOLES. REAMED HOLE IN STRINGER 2ND HOLE FROM FRONT ON BOTTOM TO 542. BEGAN DRILLING REP
- [SDR DL72S980055](https://openairdocs.org/sdr/DL72S980055.md): Bracket · cracked · Dec 20, 1997 · N403DA · Boeing 727232 · Leading Edge Devices
  > BRACKET CRACKED, ACT ATTACH BRACKET NR 3 KRUEGER FLAP OUTBD SIDE. BEGAN MANUFACTURING ANGLE REPAIR DOUBLER AS PER M/M 57-20-21 FIGURE 807. FINISH MFG ANGLE REPAIR DOUBLER PER MM 57-20-21 FIG 807. OK TO INSTALL DOUBLER. INSTALLED DOUBLER PER M/M 57-20-21 FI
- [SDR DL72S980028](https://openairdocs.org/sdr/DL72S980028.md): Frame · dented · Dec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED FS 1050 BETWEEN STR 25L AND 26L. REMOVED DAMAGE AND DYE-CHECKED PER SRM 53-10-4. NO CRACKS FOUND AROUND CUTOUT. DRILLED UP DOUBLER AS PER SRM 53-10-4 FIG 27. OK TO INSTALL, BEGAN INSTALLING REPAIR. INSTALLED PER SRM 53-10-4.
- [SDR DL72S980027](https://openairdocs.org/sdr/DL72S980027.md): Support · cracked · Dec 20, 1997 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > SUPPORTS CRACKED NR 6 L/E FLAP ACTUATOR SUPPORTS ARE CRACKED. VERIFIED CRACKS TO BE PRESENT PER PS 900-6-3. REMOVED CRACKED SUPPORTS FROM A/C. FABRICATED REPAIR PARTS PER M/M 57-20-32 FIG 807. OK TO TREAT AND PAINT TREATED AND PAINTED PER PS 900-3-6 ASSEM
- [SDR DL72S972714](https://openairdocs.org/sdr/DL72S972714.md): Frame · dented · Dec 20, 1997 · N403DA · Boeing 727232 · Fuselage Main, Frame
  > FRAME DENTED FS 1030 AT STR 26L. REPAIRED PER SRM 53-10-4 FIG 27.
- [SDR DL72S980026](https://openairdocs.org/sdr/DL72S980026.md): Liner · cracked · Dec 19, 1997 · N403DA · Boeing 727232 · Engine Cowling System
  > NR 2 ENG INLET ASSY (DOGHOUSE) ACCOUSTICAL LINER 12 O'CLOCK POS AFT CRACKED AND SEPARATING. REMOVED DAMAGED AREA, FABRICATED DOUBLER AND FILLER AS PER SRM 54-10-3 FIG 13. BEGAN INSTALLATION OF REPAIR PER SRM 54-10-3 FIG 13. COMPLETE REPAIR PER SRM 54-10-3 F
- [SDR DL72S972621](https://openairdocs.org/sdr/DL72S972621.md): Web · cracked · Dec 12, 1997 · N403DA · Boeing 727232 · Fuselage Miscellaneous Structure
  > FOUND DURING A-2 LETTER CHECK,.75 INCH CRACK LT LWR TORQUE BOX WEB STA 1227 UPPER EDGE OF VERT WEB. REPAIRED PER M/M 53-11-0.
- [SDR DL72S972620](https://openairdocs.org/sdr/DL72S972620.md): Frame · worn · Dec 12, 1997 · N403DA · Boeing 727232 · Fuselage Main, Frame
  > FOUND DURING A-2 LETTER CHECK, ANGLE WORN THROUGH 11 INCHES, 6 O'CLOCK POSITION FS 1352 FRAME. REPAIRED PER ERA 363434.
- [SDR DL72S972619](https://openairdocs.org/sdr/DL72S972619.md): Skin · cracked · Dec 12, 1997 · N403DA · Boeing 727232 · Elevator, Plate/Skin
  > FOUND DURING A-2 LETTER CHECK, 1.75 INCH CRACK IN RT ELEVATOR UPPER SKIN AT DOUBLER BETWEEN O/B 2 ELEVATOR HINGES. REPAIRED PER ERA 363435-14.
- [SDR DL72S972079](https://openairdocs.org/sdr/DL72S972079.md): Actuator · failed · Oct 16, 1997 · N403DA · Boeing 727232 · Leading Edge Slat Actuator
  > SYS-A HYDRAULIC QTY DECREASED TO ZERO IN FLT. FOUND NR 3L SLAT ACTUATOR FAILED IN RETRACT POSITION. SEALS BLOWN AT ACTUATOR ROD.
- [SDR DL72S971871](https://openairdocs.org/sdr/DL72S971871.md): Tach Gen Housing · leaking · Sep 19, 1997 · N403DA · Boeing 727232 · Engine RPM Indicating System
  > OIL TEMP NR 3 STEADILY INCREASED REACHING A MAX OF RED RADIAL. NR 3 OIL QTY STEADILY DECREASED TO APPROX 2 GALLONS. NR 3 OIL PRESSURE DROPPED TO 20 PSI SHUT DOWN ENGINE IAW CHECK LIST. FOUND OIL PUDDLED IN INTAKE. REPLACED N1 TACH GEN HOUSING AND O-RING.
- [SDR DL72S971799](https://openairdocs.org/sdr/DL72S971799.md): Battery · discharged · Sep 14, 1997 · N403DA · Boeing 727232 · Emergency Lighting
  > AFT DOOR SLIDE LIGHTS INOP. REPLACED BATT PACK, ALL EMERG LIGHTS NOW OP NORMAL.
- [SDR DL72S971111](https://openairdocs.org/sdr/DL72S971111.md): Accessory Unit · failed · Jun 9, 1997 · N403DA · Boeing 727232 · Landing Gear Position and Warning
  > BOTH PACKS OVERHEATED AND SMOKED CABIN. PACK FAN CONTROL C/B POPPED AND WOULD NOT RESET. REPLACED LANDING GEAR ACCY UNIT.
- [SDR DL72S962774](https://openairdocs.org/sdr/DL72S962774.md): Spar · cracked · Sep 19, 1996 · N403DA · Boeing 727232 · Trailing Edge Flaps
  > DURING INSPECTION, FOUND NR 2 MID FLAP AFT SPAR RAIL CRACKED. THE RAIL WAS REPAIRED PER MM 57-52-0, PG 807.
- [SDR DL72S962773](https://openairdocs.org/sdr/DL72S962773.md): Spar · cracked · Sep 19, 1996 · N403DA · Boeing 727232 · Trailing Edge Flaps
  > NR 2 MID FLAP AFT LOWER SPAR RAIL WAS FOUND CRACKED DURING INSPECTION. REPAIRED PER MM 57-52-0, PAGE 807.

Next page: https://openairdocs.org/deregistered/N403DA-2013-08-15/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 = 'N403DA' AND deregistration_id = 'N403DA-2013-08-15'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N403DA-2013-08-15/reports

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