# Service difficulty reports: N12305, cancelled Jul 14, 2003

A list on [N12305, cancelled Jul 14, 2003](https://openairdocs.org/deregistered/N12305-2003-07-14.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 · 87 reports

- [SDR EISA20000203](https://openairdocs.org/sdr/EISA20000203.md): Frame · cracked · Nov 5, 2000 · N12305 · Boeing 727231 · Fuselage Main, Frame
  > DURING SERVICE CHECK- FOUND CRACK INDICATIONS ON 620 FRAME BELOW NR 6 DOOR STOP. CORRECTIVE ACTION: FABRICATED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER AT C-1 DOOR AFT FRAME. IAW BOEING S.B. 727-53AO219, B727-200 SRM 51-40-2, 51-30-2 AND 51
- [SDR EISA20000163](https://openairdocs.org/sdr/EISA20000163.md): Frame · cracked · Sep 16, 2000 · N12305 · Boeing 727231 · Fuselage Main, Frame
  > CRACK EXTENDS FROM UNDER 5 - 10 DOWN 3 FASTENER HOLES AT 950 FRAME. REMOVED FABRICATED REPAIR DOUBLER AND TRIPLER FABRICATED REPAIR ANGLE. ALODINED, PRIMED AND INSTALLED IAW EOI-DAL-00-00096H AND B727-200 SRM 51-10-2.
- [SDR EISA20000190](https://openairdocs.org/sdr/EISA20000190.md): Angle · misdrilled · Sep 15, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 930 OPEN HOLES B/T CUSP AND STR 16L ON FRAME. INSTALLED FREEZE PLUGS FABRICATED REPAIR ANGLE AND STRAP LOCATED HOLES, PRIMED AND INSTALLED ANGLE AND STRAP REPAIR IAW TIMCO REO-W00026, B727-200 SRM 51-30-2.
- [SDR EISA20000166](https://openairdocs.org/sdr/EISA20000166.md): Fitting · cracked · Sep 15, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > PERFORMED BHFEC AT RIGHT SIDE 870 FITTING 2 HOLES HAVE CRACK INDICATIONS. STOP DRILLED, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727-200 SRM 51-10-1, 51-10-2, TIMCO REO W00024 REV A, BOEING DWG 65C35277.
- [SDR EISA20000172](https://openairdocs.org/sdr/EISA20000172.md): Mount · cracked · Sep 15, 2000 · N12305 · Boeing 727231 · Engine Mount Section
  > NR 3 ENG FWD MOUNT SUPPORT FITTING SHOW CRACKS IN HOLES C & E. REAMED HOLES, FABRICATED RADIUS FILLER AND INSTALLED FASTENERS IAW BOEING SERVICE BULLETIN 540010R4, SB 2000-5410A01 B727-200 SRM 51-10-2.
- [SDR EISA20000171](https://openairdocs.org/sdr/EISA20000171.md): Mount · cracked · Sep 15, 2000 · N12305 · Boeing 727231 · Engine Mount Section
  > NR 1 ENGINE FWD MNT SUPPORT FITTING SHOWS CRACK AT HOLES G, H, D, E, B. REAMED HOLES, FABRICATED RADIUS FILLER, ALODINED, PRIMED AND INSTALLED FASTENERS IAW BOEING SB 540010R4, SB 2000-5410A01 B727-200 SRM 51-10-2.
- [SDR EISA20000167](https://openairdocs.org/sdr/EISA20000167.md): Skin · delaminated · Sep 14, 2000 · N12305 · Boeing 727231 · Spoilers
  > NR 13 SPOILER BOARD LOWER SKIN SURFACE IS DELAMINATED. REMOVED, FABRICATED REPAIR DOUBLERS, SEALED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLERS IAW B727-200 SRM 51-10-2, 51-20-4, 51-40-6, 51-40-5 AND 57-50-2 B727-200 MM 27-61-1.
- [SDR EISA20000161](https://openairdocs.org/sdr/EISA20000161.md): Skin · corroded · Sep 13, 2000 · N12305 · Boeing 727231 · Trailing Edge Flaps
  > LT WING O/B FLAP TRAILING EDGE O/B UPPER SURFACE CORRODED. REMOVED SKIN, FABRICATED SKIN DOUBLER AND FILLER, BONDED, ALODINED, PRIMED AND SEALED IAW B727-200 SRM 51-10-1, 51-10-2, 51-20-4, 51-40-5, 51-40-6 AND 57-50-2.
- [SDR EISA20000164](https://openairdocs.org/sdr/EISA20000164.md): Spar · corroded · Sep 12, 2000 · N12305 · Boeing 727231 · Wing Spar
  > RT WING AFT SPAR UPPER CHORD CORRODED 15 INCHES I/B OF O/B FLAP O/B TANS AT APPROX WS 626. REMOVED, FABRICATED 2 Z-STIFFENERS AND FILLERS AND ANGLES LOCATED, DRILLED, DEBURRED, AND INSTALLED IAW B727-200 SRM 51-10-2, 51-10-6, 51-30-2, 57-10-6, 57-10-1 AND MM
- [SDR EISA20000162](https://openairdocs.org/sdr/EISA20000162.md): Skin · cracked · Sep 9, 2000 · N12305 · Boeing 727231 · Leading Edge Devices
  > RT WING NR 5 SLAT I/B HOOK SEAL CUTOUT L/E SKIN HAS CRACKS BOTH CORNERS. FABRICATED FILLER AND DOUBLER, PASSIVATED, PRIMED AND INSTALLED IAW B727-200 SRM 57-30-4 AND 51-30-2.
- [SDR EISA20000168](https://openairdocs.org/sdr/EISA20000168.md): Skin · delaminated · Sep 7, 2000 · N12305 · Boeing 727231 · Trailing Edge Flaps
  > RT WING INBOARD AFT FLAP IS DELAMINATED. REMOVED, FABRICATED SKIN FILLER AND DOUBLER, ALODINED, PRIMED, BONDED AND SEALED SKIN FILLER AND DOUBLER IAW B727-200 SRM 51-10-1, 51-10-2, 51-20-1 PG 13, 51-40-5, 51-40-6 AND 51-20-4.
- [SDR EISA20000179](https://openairdocs.org/sdr/EISA20000179.md): Strap · cracked · Sep 6, 2000 · N12305 · Boeing 727231 · Flight Compartment Windows
  > PERFOMRED X-RAY OF RT SIDE COCKPIT WINDOW POST CRACKS NOTED. REMOVED, LOCATED, DRILLED AND INSTALLED WINDOW POST IAW BOEING DWG 65-87208 AND B727-200 SRM 51-30-2.
- [SDR EISA20000158](https://openairdocs.org/sdr/EISA20000158.md): Stiffener · corroded · Sep 6, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > FWD E&E COMPARTMENT LT VERTICAL STIFFENER AT RBL 14, BS 344 AT WL 168 CORRODED. REMOVED, FABRICATED REPAIR DOUBLER, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727-200 SRM 51-10-2, 51-30-2, AND 53-10-1.
- [SDR EISA20000165](https://openairdocs.org/sdr/EISA20000165.md): Skin · corroded · Sep 4, 2000 · N12305 · Boeing 727231 · Fuselage Main, Plate/Skin
  > T/H FWD E&E COMPARTMENT AT FS 294 - 312, RBL 20 CORRODED TOP WHEEL WELL. REMOVED, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED DOUBLER IAW B727-200 SRM 51-10-6, 51-10-2 AND 51-20-1 AND 51-30-2.
- [SDR EISA20000178](https://openairdocs.org/sdr/EISA20000178.md): Beam · cracked · Sep 2, 2000 · N12305 · Boeing 727231 · Fuselage Main, Structure
  > PERFORMED HFEC LOCATED CRACK AT BS1050 AND STR 26R. CORRECTIVE ACTION: REMOVED, FABRICATED, REPAIR DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 51-30-2, 53-10-2 AND 53-10-4.
- [SDR EISA20000177](https://openairdocs.org/sdr/EISA20000177.md): Floorbeam · gouged · Sep 1, 2000 · N12305 · Boeing 727231 · Fuselage Main, Floor Beam
  > FLOORBEAM AT STA 990 LBL 70, UPPER CHORD, AFT FLANGE GOUGED. REMOVED, FABRICATED REPAIR DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-8.
- [SDR EISA20000174](https://openairdocs.org/sdr/EISA20000174.md): Angle · cracked · Sep 1, 2000 · N12305 · Boeing 727231 · Nacelle/Pylon, Main Frame
  > NR 1 ENGINE NOSE COWL AFT SECTION AT BULKHEAD FLANGE CRACKED. REMOVED, FABRICATED REPAIR ANGLE AND FILLER, DRILLED, DEBURRED, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 54-10-3.
- [SDR EISA20000157](https://openairdocs.org/sdr/EISA20000157.md): Clip · cracked · Sep 1, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > STR 8L END TIE IS CRACKED AT STA 950. REMOVED AND REPLACED END TIE IAW B727-200 SRM, 51-10-1, AND 51-30-2.
- [SDR EISA20000173](https://openairdocs.org/sdr/EISA20000173.md): Fitting · cracked · Aug 31, 2000 · N12305 · Boeing 727231 · Landing Gear Doors
  > PERFORMED BHFEC AT FLAP TRACK LANDING GEAR DOOR FED HINGE FITTING ATTACHMENT HOLES LT AND RT SIDE 7 HOLES TOTAL. REAMED HOLES PER BOEING SB 727-32-0340.
- [SDR EISA20000160](https://openairdocs.org/sdr/EISA20000160.md): Skin · separated · Aug 31, 2000 · N12305 · Boeing 727231 · Ailerons
  > LEFT WING O/B AILERON O/B TRAILING EDGE CORNER METAL SEPARATED. REMOVED, FABRICATED SKIN DOUBLERS AND FILLERS, BONDED, ALODINED, AND PRIMED SKIN DOUBLERS AND FILLERS IAW B727-200 SRM 51-10-, 51-20-1, 51-40-5, 51-40-6, 57-50-2 AND B727-200 MM 51-20-151.
- [SDR EISA20000159](https://openairdocs.org/sdr/EISA20000159.md): Skin · gouged · Aug 31, 2000 · N12305 · Boeing 727231 · Ailerons
  > LT WING O/B AILERON T/E LOWER SURFACE HAS GOUGE. REMOVED, FABRICATED REPAIR DOUBLERS AND FILLERS, BONDED, ALODINED, PRIMED IAW B727-200 SRM 51-10-2, 51-20-1, 51-40-5, 51-40-6, 57-50-2, AND B727-200 MM 51-20-151.
- [SDR EISA20000175](https://openairdocs.org/sdr/EISA20000175.md): Fitting · cracked · Aug 31, 2000 · N12305 · Boeing 727231 · Fuselage Main, Attach Fittings
  > PERFORMED HFEC ON FWD LANDING GEAR DOOR HINGE FITTING FOUND CRACKS TOTAL OF 8 HOLES LT AND RT SIDE. REAMED ALL SIDES, CLEANED, SHOT PEENED FITTINGS, ALODINED, PRIMED AND INSTALLED IAW B727 SRM 51-10-2, SOPM 20-10-03 AND SB 727-32-0340.
- [SDR EISA20000169](https://openairdocs.org/sdr/EISA20000169.md): Floorbeam · corroded · Aug 28, 2000 · N12305 · Boeing 727231 · Fuselage Main, Floor Beam
  > FLOORBEAM SUPPORT STRAP AT BS 1030 TO BS 1070 BL 72R CORRODED. REMOVED, FABRICATED STRAP SPLICE, ALODINED, PRIMED AND INSTALLED STRAP SPLICE IAW B727-200 SRM 51-10-2 AND 53-10-3.
- [SDR EISA20000189](https://openairdocs.org/sdr/EISA20000189.md): Doubler · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 560 CRACKED B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR DOUBLER AND FILLER ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.
- [SDR EISA20000188](https://openairdocs.org/sdr/EISA20000188.md): Angle · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 580 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED, FABRICATED REPAIR ANGLE ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.
- [SDR EISA20000187](https://openairdocs.org/sdr/EISA20000187.md): Doubler · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 620 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED FABRICATED PLATES AND FILLER, ALODINED, PRIMED AND INSTALLED PLATES AND FILLER IAW B727-200 SRM 51-10-2 AND 51-40-4.
- [SDR EISA20000186](https://openairdocs.org/sdr/EISA20000186.md): Doubler · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 640 CRACKED B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR DOUBELR, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.
- [SDR EISA20000170](https://openairdocs.org/sdr/EISA20000170.md): Splice · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > STR 22R BETWEEN BS 380 - 400, CRACKED. REMOVED FABRICATED SPLICE, ALODINED, PRIMED AND INSTALLED REPAIR SPLICE IAW B727-200 SRM 51-10-2, 51-10-6 AND 53-10-3.
- [SDR EISA20000176](https://openairdocs.org/sdr/EISA20000176.md): Angle · cracked · Aug 26, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 540 CRACKED B/T CUSP AND STR 16R ON FRAME. REMOVED SECTION, FABRICATED ANGLE REPAIR, ALODINED, PRIMED AND INSTALLED ANGLES REPAIR IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.
- [SDR EISA20000185](https://openairdocs.org/sdr/EISA20000185.md): Doubler · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 720E DRILLED HOLE IN RADIUS B/T CUSP AND STR 16R ON FRAME. REMOVED FABRICATED DOUBLER AND FILLER, FORMED, DRILLED, DEBURRED, ALODINED AND PRIMED AND INSTALLED REPAIR DOUBLER AND FILLER IAW B727-200 SRM 51-10-2 AND 53-10-4.
- [SDR EISA20000184](https://openairdocs.org/sdr/EISA20000184.md): Angle · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 950F DRILLED HOLES IN RADIUS B/T CUSP AND STR 16R ON FRAME. FABRICATED REPAIR ANGLE, ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2 AND 53-10-4.
- [SDR EISA20000183](https://openairdocs.org/sdr/EISA20000183.md): Frame · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Main, Frame
  > BS 970 DRILLED HOLE IN RADIUS B/T CUSP AND 16R ON FRAME. ROUNDED HOLE IN RADIUS, FABRICATED REPAIR DOUBLER, ALODINED, PRIMED AND INSTALLED REPAIR DOUBLER IAW B727-200 SRM, 51-10-2, 51-40-3 AND 53-10-2.
- [SDR EISA20000182](https://openairdocs.org/sdr/EISA20000182.md): Angle · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 1110 TRIPLE DRILLED HOLE BT CUSP AND STR 16R ON FRAME. REMOVED, FABRICATED REPAIR ANGLE AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2 AND 53-10-4.
- [SDR EISA20000181](https://openairdocs.org/sdr/EISA20000181.md): Doubler · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Main, Structure
  > BS 950D DRILLED HOLE IN RADIUS B/T CUSP AND STR 16L /IB FRAME. REMOVED, FABRICATED DOUBLER AND FILLER, ALODINED, PRIMED AND INSTALLED IAW B727-200 SRM 51-10-2 AND 53-10-4.
- [SDR EISA20000180](https://openairdocs.org/sdr/EISA20000180.md): Angle · misdrilled · Aug 25, 2000 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > BS 1110 DRILLED HOLE IN RADIUS B/T CUSP AND STR 16L I/B FRAME. REMOVED, FABRICATED ANGLE REPAIR, ALODINED, PRIMED AND INSTALLED REPAIR ANGLE IAW B727-200 SRM 51-10-2, 51-30-2 AND 53-10-4.
- [SDR EISA20000125](https://openairdocs.org/sdr/EISA20000125.md): Door · not closed · Aug 15, 2000 · N12305 · Boeing 727231 · Passenger/Crew Doors
  > AIRCRAFT WOULD NOT MAINTAIN PRESSURE. AIR TURNBACK TO (CVG). VISUALLY INSPECTED EXTERIOR DOORS FOR SECURITY, FOUND VAULT DOOR HANDLE CLOSED, BUT DOOR NOT FULLY CLOSED. CYCLED DOOR SEVERAL TIMES, LIGHT AND DOOR OPS CHECK NORMAL.
- [SDR EISA20000105](https://openairdocs.org/sdr/EISA20000105.md): Accumulator · leaking · Aug 10, 2000 · N12305 · Boeing 727231 · Hydraulic Power Accumulator, Main
  > TEN MINUTES AFTER TAKEOFF A SYSTEM HYDRAULIC PRESSURE DROPPED TO 1000 PSI AND SYSTEM FLUID QUANTITY DROPPED TO O, SEE LOG PAGE 60983 REPEAT WRITE UP. REMOVED AND REPLACED A SYSTEM ACCUMULATOR, NR 1, NR 2, ENGINE HYDRAULIC PUMPS, IAW M/M 29-00, OPS CHECK NORMA
- [SDR EISA20000104](https://openairdocs.org/sdr/EISA20000104.md): Accumulator · low · Aug 9, 2000 · N12305 · Boeing 727231 · Hydraulic Power Accumulator, Main
  > AFTER 25 MINUTE OF FLIGHT A HYDRAULIC SYSTEM FLUID LEVEL WENT TO ZERO, BOTH PUMP LOW PRESSURE LIGHTS CAME ON. AIR TURN BACK TO ELP. REMOVED AND REPLACED A SYSTEM PUMP FILTERS, NO CONTAMINATION FOUND. REPLACED A SYSTEM ACCUMALATOR IAW M/M 29-00, OPS CHECK NO
- [SDR EISA2000008](https://openairdocs.org/sdr/EISA2000008.md): Switch · shorted · Jan 22, 2000 · N12305 · Boeing 727231 · Cabin Pressure Control System
  > DURING CLIMB, DUCT USING RIGHT PACK ONLY, WERE UNABLE TO MAINTAIN PRESSURIZATION ABOVE FL 20,000. AIR TURN BACK TO BRUSSELS. REMOVED AND REPLACED PACK SWITCH. (M)
- [SDR EISA99084](https://openairdocs.org/sdr/EISA99084.md): Light · loose · Apr 6, 1999 · N12305 · Boeing 727231 · Emergency Lighting
  > EMERGENCY EXIT LIGHT FALLS OFF FORWARD ENTRY DOOR AND WILL NOT STAY ATTACHED. ALSO, LIGHT IS DISCHARGED. REMOVED AND REPLACED FORWARD ENTRY EXIT LIGHT. SECURITY AND OPS CHECK GOOD PE RMM 33-50-0. (M)
- [SDR EISA99015](https://openairdocs.org/sdr/EISA99015.md): Pneumatic Line · fractured · Jan 20, 1999 · N12305 · Boeing 727231 · Pneumatic Distribution System
  > NR 3 ENGINE STRUT OVERHEAT LIGHT ILLUMINATED IN FLIGHT AFTER TAKEOFF. FOUND HOLE IN BRAIDED HIGH PRESSURE LINE IN THE ENGINE STRUT AREA. REMOVED AND REPLACED LINE IAW MM 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW 26-14 MM. (M)
- [SDR EISA99007](https://openairdocs.org/sdr/EISA99007.md): Pneumatic Line · punctured · Jan 20, 1999 · N12305 · Boeing 727231 · Pneumatic Distribution System
  > NR 3 ENGINE STRUT OVERHEATS IN FLIGHT AFTER TAKEOFF. FOUND BRAIDED HP AIR LINE HOLE ENGINE STRUT. REMOVED AND REPLACED LINE IAW MM CHAPTER 36-12. LEAK AND OPS CHECK GOOD ON GROUND IAW MM 26-14. (M)
- [SDR EISA98140](https://openairdocs.org/sdr/EISA98140.md): Structure · corroded · Jun 12, 1998 · N12305 · Boeing 727231 · Fuselage Main, Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK CARD NR 269, INSPECTION OF PLENUM CHAMBERS. OBSERVED CORROSION AT STR S4C AND LBL 29.9 AND LBL 31.8 AND STR S3C RBL 16.5 AND STR S4C AT RBL 32.0. BOEING REPAIR NR EOIR980527 AND EOIR980529. (X)
- [SDR EISA98129](https://openairdocs.org/sdr/EISA98129.md): Fitting · mismanufactured · Jun 12, 1998 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD 045R, FOUND RIGHT HAND 740 FITTING CRACKED. DURING REPLACEMENT OF 740 FITTING, FOUND THAT REPLACEMENT FITTING WAS DIFFERENT. THE EDGE DISTANCE WAS TOO CLOSE. BOEING ENGINEERING SUPPLIED DRAWING AND INFORMAT
- [SDR EISA98133](https://openairdocs.org/sdr/EISA98133.md): Frame · cracked · May 27, 1998 · N12305 · Boeing 727231 · Fuselage Main, Frame
  > DURING ACCOMPLISHMENT OF ROUTINE C-CHECK WORK CARD SEQ 237, RIGHT SIDE STA 760.95 FOUND FRAME CRACKED. INSTALLED BOEING REPAIR KIT PER SB 53-0197. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)
- [SDR EISA98132](https://openairdocs.org/sdr/EISA98132.md): Fitting · cracked · May 27, 1998 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURNG ACCOMPLISHMENT OF ROUTINE WORK CARD 045 OR SB 53-62 R6, INSPECTION OF 740 FITTINGS FOUND RIGHT HAND 740 FITTING CRACKED. REPLACED RIGHT-HAND 740 FITTING PER SB 53-0062. USED BOEING KIT 65C13724-96. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)
- [SDR EISA98131](https://openairdocs.org/sdr/EISA98131.md): Rib · cracked · May 27, 1998 · N12305 · Boeing 727231 · Wing, Rib/Bulkhead
  > DURING ACCOMPLISHMENT OF ROUTINE WORK CARD FOR C-CHECK SEQ 237, FOUND UPPER RIB CHORD CRACKED AT BBL 70.5 STA 760.95 ON LEFT HAND SIDE OF AIRCRAFT. INSTALLED REPAIR KIT PER SB 57-112 R5. ACFT TT: 65,287:32 HOURS. ACFT TC: 44,162. (X)
- [SDR EISA98130](https://openairdocs.org/sdr/EISA98130.md): Fitting · cracked · May 27, 1998 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > DURING ACCOMPLISHMENT OF C-CHECK, CPCP CARD NR C53-100-01, BS 1170 LEFT HAND SIDE AT AFT LAV DOOR AREA STR 20 FOUND BULGE, OPENED SKIN FOUND CRACK AND CORROSION ON FITTING. REMOVED CORROSION AND REPLACED STRINGER PER MM 53-10-3. ACFT TT: 65,287:32 HOURS. A
- [SDR EISA97229](https://openairdocs.org/sdr/EISA97229.md): Connector · loose · Nov 27, 1997 · N12305 · Boeing 727231 · Flight Compartment Lighting
  > FWD INST BACK GROUND LIGHTS INOP ALSO TWO WHITE EMERGENCY ON CONTINUOUSLY EVEN WITH ESSENTIAL AC BUS POWERED. REPAIRED PIN AND CANNON PLUG AT F/O'S PANEL TO GLARESHIELD. (M)
- [SDR EISA97259](https://openairdocs.org/sdr/EISA97259.md): Support · corroded · Nov 24, 1997 · N12305 · Boeing 727231 · Fuselage Miscellaneous Structure
  > MAIN CABIN - RT SIDE FS 420 FLOOR SUPPORT HAS CORROSION. FLOOR SUPPORT REMOVED AND NOT USED DUE TO CARGO MOD PER STC SA 1798-SO AND DRAWING NR AE 727-2-063. TT: 64,924 HOURS. TC: 43,819. X)

Next page: https://openairdocs.org/deregistered/N12305-2003-07-14/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 = 'N12305' AND deregistration_id = 'N12305-2003-07-14'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/deregistered/N12305-2003-07-14/reports

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