# Service difficulty reports: Boeing 727-2S7

A list on [Boeing 727-2S7](https://openairdocs.org/model/boeing-727-2s7.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 12 · 555 reports

- [SDR C1HA200881001](https://openairdocs.org/sdr/C1HA200881001.md): Engine · erratic · Apr 11, 2008 · N681CA · Boeing 7272S7 · Engine (Turbine/Turboprop)
  > NR 1 ENGINE ENGINE CONTINUOUS ERRATIC AT ALT EPR - N1 - N2 TEMP DECREASING AND SURGING. RETURNED FOR LANDING HOUSTON. REPLACED NR 1 ENG FUEL FILTER AND DID FIND CONTAMINATION. REPLACED 2 AND 3 ENG FILTERS PRECAUTIONARY PER 73-11-01, 405. PERFORMED ENG RUN
- [SDR C1HA200883001](https://openairdocs.org/sdr/C1HA200883001.md): Skin · dented · Jan 14, 2008 · N683CA · Boeing 7272S7 · Fuselage Main, Plate/Skin
  > DENT AT BS 388 ON STR 22R TASK CARD E99683-1.4 DUE TEMP REPAIR AT DENT IN FUSE STA AT BS 338 AND S-22R VERIFIED HFEC INSPECTION OF DENT AND STRINGER HAS BEEN ACCOMPLISHED ON WO 122987 AND THAT NO CRACKS WERE FOUND. TEMP REPAIRED PER TASK CARD E99683-14. ACCO
- [SDR C1HA200786006](https://openairdocs.org/sdr/C1HA200786006.md): Relief Valve · failed · Oct 8, 2007 · N686CA · Boeing 7272S7 · Cabin Pressure Controller
  > UNABLE TO CONTROL CABIN PRESSURE WITH ANY MODE OF CONTROLLER. REMOVED AND REPLACED OUT FLOW VALVE IAW MM 21-31-11, PERFORMED ADJ TEST IAW MM 21-31-00, OPS CHECK NORMAL. IN ALL MODES OF PRESSURIZATION, CABIN PRESSURE/ALTITUDE CLIMBS WHEN DIFF PRESS HITS 7.7 P
- [SDR C1HA200786005](https://openairdocs.org/sdr/C1HA200786005.md): Floorbeam · corroded · Oct 1, 2007 · N686CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM AT BS 1035 LBL 24-45. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTALLED NEW PART IAW B727 SRM 51-30-2 FIG 1 AND 3.
- [SDR C1HA200786004](https://openairdocs.org/sdr/C1HA200786004.md): Seat Track · corroded · Oct 1, 2007 · N686CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON TRACK ANGLE AT BS 1033 LBL 54.5. REMOVED EXISTING PART, FABRICATED NEW PART; TREATED AND PRIMED AND INSTALLED NEW PART IAW B727 SRM 51-30-2 FIG 1 AND 13.
- [SDR C1HA200786003](https://openairdocs.org/sdr/C1HA200786003.md): Floorbeam · corroded · Oct 1, 2007 · N686CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > NUMEROUS AREAS OF CORROSION ON FLOOR BEAM AT BS 344 LBL 25 - RBL 6. CUT OUT DAMAGED AREA. FABRICATED REPAIR PARTS AND INSTALLED REPAIR PARTS IAW B727 SRM 53-10-8 FIG 9.
- [SDR C1HA200786002](https://openairdocs.org/sdr/C1HA200786002.md): Floorbeam · corroded · Oct 1, 2007 · N686CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > BS 1030 FLOORBEAM CORROSION LBL 25 - RBL 25 TOP SURFACE UPPER CHORD. REMOVED AND REPLACED PREVIOUS UPPER "T" CHORD REPAIR IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200786001](https://openairdocs.org/sdr/C1HA200786001.md): Floorbeam · corroded · Oct 1, 2007 · N686CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > BS 1110 FLOORBEAM CORROSION LBL 45 - RBL 45 TOP SURFACE UPPER CHORD. REPAIR BS 1110 FLOORBEAM IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200781001](https://openairdocs.org/sdr/C1HA200781001.md): Skin · corroded · Sep 20, 2007 · N681CA · Boeing 7272S7 · Wing, Center Box
  > WING CENTER SECTION LWR SKIN CORROSION, LT PRIMARY HEAT EXCHANGER PLENUM AREA. REMOVED CORROSION AND FOUND OUT OF LIMITS IAW B727 SRM 57-30-1 FIG 4. REPAIRED IAW CHAMPION AIR, EO-727-5710-05.
- [SDR C1HA200781005](https://openairdocs.org/sdr/C1HA200781005.md): Seat Track · corroded · Sep 20, 2007 · N681CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK BS 344 -480 LBL 25. REMOVED AND REPLACED SEAT TRACK BS 344 - 480 LBL 25 IAW B727 SRM 53-10-2 AND 53-10-5
- [SDR CIHA200781004](https://openairdocs.org/sdr/CIHA200781004.md): Seat Track · corroded · Sep 20, 2007 · N681CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION SEAT TRACK BS 344 - 480 LBL 45. REMOVED AND REPLACED SEAT TRACK BS 344 - 480 LBL 45 IAW B727 SRM 53-10-2 FIG. 7 AND 53-10-5
- [SDR C1HA200781003](https://openairdocs.org/sdr/C1HA200781003.md): Floorbeam · corroded · Sep 20, 2007 · N681CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > CORROSION ON FLOORBEAM BS 380 BL O TO RBL 45. FABRICATED REPAIR FOR FLOOR BEAM BS 380 BL-O TO RBL - 45- AND INSTALLED IAW B727 53-10-8 FIG 3.
- [SDR C1HA200781002](https://openairdocs.org/sdr/C1HA200781002.md): Seat Track · corroded · Sep 20, 2007 · N681CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CORROSION ON SEAT TRACK RBL 25-BS 400 - 420. REMOVED AND REPLACED SEAT TRACK RBL 25 BS 400 - 420 IAW B727 SRM 53-10-2 AND 53-10-5 FIG 7.
- [SDR C1HA200781006](https://openairdocs.org/sdr/C1HA200781006.md): Frame · cracked · Sep 20, 2007 · N681CA · Boeing 7272S7 · Fuselage Main, Frame
  > BS 1183 VERT FRAME RBL 35 WL 233 CRACK IN AFT RADIUS. STOP DRILLED CRACK AND INSTALLED REPAIR PARTS PER S/B 727-53-0192 REV 1 DATED 5/30/91.
- [SDR C1HA200785001](https://openairdocs.org/sdr/C1HA200785001.md): Threshold · cracked · Jun 21, 2007 · N685CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > FLIGHT ATTENDANTS REPORTED VIBRATION IN FLOOR IN FRONT OF AFT ENTRY DOOR AND GRINDING NOISE. ON DESCENT PULLED POWER LEVERS TO IDLE CABIN STARTED TO CLIMB AND NOISE AND VIBRATION WENT AWAY, WHEN POWER LEVERS ADVANCED CABIN DESCENDED AND VIBRATION AND NOISE RE
- [SDR C1HA200681004](https://openairdocs.org/sdr/C1HA200681004.md): Csd · failed · Nov 23, 2006 · N681CA · Boeing 7272S7 · Alternator-Generator Drive
  > CSD LOW OIL PRESSURE LIGHT ILLUMINATED W/ NR 2 CB ILLUMINATED. CSD OIL TEMP OFF SCALE HIGH IN THE IN POSITION. RESIDUAL VOLTS 55. PERFORMED COM 2.24.15 AND 2.26.2 PRECAUTION ENGINE SHUTDOWN. REMOVED AND REPLACED NR 2 CSD IAW 24-10-11. REMOVED AND REPLACED
- [SDR C1HA200682019](https://openairdocs.org/sdr/C1HA200682019.md): Wire · broken · Nov 16, 2006 · N682CA · Boeing 7272S7 · Flight Control System Wiring
  > "UPON RETRACTION OF FLAPS AFTER TAKEOFF, AMBER NR 7 LEADING EDGE LIGHT REMAINED ILLUMINATED, RUN COM PROCEDURE 2.27.12, DUMPED FUEL RETURN TO DEW. REMOVED AND REPLACED NR 7 SLAT ACTUATOR PER MM 27-81-32, OPS CHECK LEAK CHECK OK WHILE RARE ACTUATOR MX FOUND FO
- [SDR C1HA200682018](https://openairdocs.org/sdr/C1HA200682018.md): Shutoff Valve · failed · Oct 11, 2006 · N682CA · Boeing 7272S7 · Pneumatic Indicating System
  > AT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 WAS PERFORMED,THE 33 BLEED AIR VALVE WAS CLOSED, AND THE RT DUCT PRESSURE REMAINED AT 10 PSI. THE NR
- [SDR C1HA200682017](https://openairdocs.org/sdr/C1HA200682017.md): Bleed Valve · failed · Oct 11, 2006 · N682CA · Boeing 7272S7 · Compressor Bleed Valve
  > AT FL350 THE NR 3 BLEED AIR TRIP OFF LT ILLUMINATED.THE RT DUCT PRESSURE NEEDLE DROPPED FROM APPROX 24 PSI TO 10 PSI AND THE CABIN STARTED TO CLIMB. COM 2.36.2 WAS PERFORMED,THE 33 BLEED AIR VALVE WAS CLOSED, AND THE RT DUCT PRESSURE REMAINED AT 10 PSI.THE N
- [SDR C1HA200685012](https://openairdocs.org/sdr/C1HA200685012.md): Motor · failed · Aug 10, 2006 · N685CA · Boeing 7272S7 · Trailing Edge Flap Control System
  > ON CLIMB FROM DFW ALL OF -A- SYSTEM HYD WAS LOST, COMPLIED WITH COM 2.29-2. RETURNED TO DFW. REMOVED AND REPLACED O/B FLAP DRIVE MOTOR PER MM 27-51-62, ALL TEST NORMAL. DUE TO -A- SYS HYD LOSE REPLACE NR 1 & 2 -A- SYS HYD PUMPS & FILTERS. REMOVED & REPLACE
- [SDR C1HA200683003](https://openairdocs.org/sdr/C1HA200683003.md): Stringer · corroded · May 24, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Longeron/Stringer
  > STRINGER 25R BS 331 CORRODED. REMOVED & REPLACED DAMAGED STRINGER IAW 727 SRM 51-30-2.
- [SDR C1HA200683020](https://openairdocs.org/sdr/C1HA200683020.md): Stringer · corroded · May 24, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Longeron/Stringer
  > STRINGER 23L CORRODED AT BS 1179. REPAIRED CORRODED STRINGER 23L AT BS 1179 IAW 727 SRM 53-10-3 FIG 1.
- [SDR C1HA200683021](https://openairdocs.org/sdr/C1HA200683021.md): Stringer Clip · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Attach Fittings
  > STRINGER 23L TENSION TIE AT BS 1183 CORRODED. REMOVED & REPLACED TENSION TIE IAW B727 SRM 51-30-2. FABBED & INSTALLED ACCESS DOUBLER IAW B727 SRM 53-30-3 FIG 26.
- [SDR C1HA200683010](https://openairdocs.org/sdr/C1HA200683010.md): Intercostal · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE BETWEEN BS 320-340 HAS FLANGE SUPPORT STIFFENER WITH CORROSION, RBL 44. REMOVED AND REPLACED FLOOR SUPPORT INTERCOSTAL AT MAIN CABIN BS 320-340, RBL 44, IAW B727 SRM 51-40-4.
- [SDR C1HA200683018](https://openairdocs.org/sdr/C1HA200683018.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45, BS 500 WITH DEEP CORROSION. REPLACED SEAT TRACK SECTION FROM BS 500 TO 480, LBL 45 IAW B727 SRM 53-10-5.
- [SDR C1HA200683009](https://openairdocs.org/sdr/C1HA200683009.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK END FITTING AT LBL 55, BS 1030 CORRODED. REMOVED AND REPLACED SEAT TRACK AT BS 1030-990, LBL 55 IAW B727 SRM 51-30-2 AND 53-10-5.
- [SDR C1HA200683008](https://openairdocs.org/sdr/C1HA200683008.md): Floorbeam · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > MAIN CABIN FLOORBEAM CORRODED AT BS 1030, LBL 45. REPAIRED FLOORBEAM AT BS 1030, LBL 45 IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200683011](https://openairdocs.org/sdr/C1HA200683011.md): Floor Support · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > CABIN FLOOR STRUCTURE BETWEEN BS 320-360 AT RBL 50, HAS SIDEWALL STIFFENER WITH CORROSION. REPLACED MAIN CABIN FLOOR ANGLE RBL 50 IAW B727 SRM 51-40-3.
- [SDR C1HA200683019](https://openairdocs.org/sdr/C1HA200683019.md): Skin · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON FUSELAGE SKIN AT DOME NUTS BETWEEN BS 700-720 AT STR 28L-27R. REPAIRED AREA IAW B727 SRM 53-30-3 FIG 1 AND CHAMPION AIR DWG GRD 727-5170-001 REV NC DATED 8 NOV 02.
- [SDR CIHA200683016](https://openairdocs.org/sdr/CIHA200683016.md): Intercostal · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > STA 312, RBL 56 INTERCOSTAL WITH CORROSION. REMOVED AND REPLACED INTERCOSTAL IAW B727 SRM 51-30-2.
- [SDR CIHA200683015](https://openairdocs.org/sdr/CIHA200683015.md): Intercostal · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > STA 312 RBL 45 OUTBOARD INTERCOSTAL WITH CORROSION. REMOVED AND REPLACED INTERCOSTAL IAW B727 SRM 51-30-2.
- [SDR C1HA200683014](https://openairdocs.org/sdr/C1HA200683014.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > STA 1130 TO 1070 LBL 55 SEAT TRACK CORRODED. REPLACED SEAT TRACK LBL 45 FROM BS 1130 TO 1070 IAW B727 SRM 53-10-5.
- [SDR C1HA200683013](https://openairdocs.org/sdr/C1HA200683013.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > AFT GALLEY AREA AT LBL 45, BS 1070 TO 1110 HAS CORROSION. REPAIRED SECTION OF SEAT TRACK AT BS 1030, BETWEEN 960 TO 1030, LBL 45, IAW B727 SRM 53-10-5.
- [SDR C1HA200683023](https://openairdocs.org/sdr/C1HA200683023.md): Vertical Beam · cracked · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Bulkhead
  > STA 1183 BULKHEAD VERTICAL BEAM RBL 36 IS CRACKED AT WL 238. STOP DRILLED CRACK AND REPAIRED PER S/B 727-53-0192 REV 1 DATED MAY 30, 1991 P/N 65C34406-15 PO 623137.
- [SDR C1HA200683007](https://openairdocs.org/sdr/C1HA200683007.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > AFT GALLEY AREA AT LBL 24, BS 1110 HAS CORROSION AT SEAT TRACK. REMOVED AND REPLACED SEAT TRACK FROM BS 1030 TO 1130, LBL 24 IAW B727 SRM 53-10-5.
- [SDR C1HA200683006](https://openairdocs.org/sdr/C1HA200683006.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE AT BS 400, LBL 24 HAS SEAT TRACK WITH CORROSION. REPLACED SEAT TRACK FROM 340 TO 480, LBL 24 IAW B727 SRM 53-10-5.
- [SDR C1HA200683005](https://openairdocs.org/sdr/C1HA200683005.md): Floorbeam · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > CABIN FLOORBEAM AT BS 1110, LBL 20 HAS CORROSION ON TOP FLANGE. REPAIRED FLOORBEAM AT BS 1110 LBL 20 IAW B727 SRM 53-10-8 FIG 3.
- [SDR C1HA200683012](https://openairdocs.org/sdr/C1HA200683012.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > CABIN FLOOR STRUCTURE AT BS 420 SEAT TRACK HAS CORROSION BOTTOM SIDE OF FLANGE, RBL 44. REPLACED SEAT TRACK FROM BS 340 TO 480, RBL 45 IAW B727 SRM 53-10-5 FIG 1.
- [SDR C1HA200683004](https://openairdocs.org/sdr/C1HA200683004.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > AFT GALLEY AREA LBL 45.0 BS 1070 TO 1110 HAS CORROSION. REPLACED SEAT TRACK FROM 1030 TO 1130 LBL 45 IAW B727 SRM 53-10-5.
- [SDR C1HA200683017](https://openairdocs.org/sdr/C1HA200683017.md): Seat Track · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > SEAT TRACK AT LBL 45, BS 405 WITH CORROSION. REPLACED SEAT TRACK BETWEEN BS 380 TO 480, LBL 45, IAW B727 SRM 53-10-5.
- [SDR C1HA200683002](https://openairdocs.org/sdr/C1HA200683002.md): Channel · corroded · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > C-CHANNEL AT BS 304 RBL 14.6 CORRODED. REPLACED DAMAGED C-CHANNEL (STIFFENER) P/N 65-18915-266 PO 6231140 IAW 727 SRM 51-30-2 & 51-10-1.
- [SDR C1HA200683022](https://openairdocs.org/sdr/C1HA200683022.md): Vertical Beam · cracked · May 22, 2006 · N683CA · Boeing 7272S7 · Fuselage Main, Bulkhead
  > STA 1183 BULKHEAD VERTICAL BEAM AT LBL 36 IS CRACKED AT WL 238. REPAIRED VERTICAL BEAM AT LBL 36 BS 1183 IAW S/B 727-53-0192, REV 1 DATED MAY 1992.
- [SDR C1HA200685001](https://openairdocs.org/sdr/C1HA200685001.md): Seat Track · corroded · May 10, 2006 · N685CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN SEAT TRACK AT RBL 45 HAS CORROSION AT STA 480. FOUND CORROSION OUT OF LIMITS IAW B727 SRM 53-10-1. REMOVED SEAT TRACK IAW B727 SRM 51-30-2, FABRICATED NEW TRACK USING BAC 1520-792-7178 IAW B727 SRM 53-10-2, ALODINE & PRIME IAW B727 SRM 51-10-2.
- [SDR CIHA200685011](https://openairdocs.org/sdr/CIHA200685011.md): Floorbeam · corroded · May 10, 2006 · N685CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > CORROSION CABIN FLOORBEAM LBL 10 TO 20 STA 360. FOUND CORROSION OUT OF LIMITS. CUT OUT DAMAGED AREA IAW B727 SRM 51-10-0. FAB 2EA ANGLE REPAIRS FROM BAC1490-2888 7075 T6IAW B727 SRM 53-10-8 FIG 8. ALODINE & PRIME IAW B727 SRM 51-10-2, INSTALLED PARTS IAW B
- [SDR C1HA200685010](https://openairdocs.org/sdr/C1HA200685010.md): Floorbeam · corroded · May 3, 2006 · N685CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > UPPER CABIN FLOOR ANGLE AT STA 1179 RBL 45 TO RBL 65 HAS AREAS OF CORROSION. CLEANED AREA IAW B727 SRM 53-10-0. REMOVED WEB IAW B727 SRM 51-30-2. CORROSION FOUND OUT OF LIMITS, ORIGINAL THICKNESS OF 0.300, MATERIAL LOSS 0.045, MATERIAL REMAINING 0.255 IAW
- [SDR C1HA200685009](https://openairdocs.org/sdr/C1HA200685009.md): Stiffener · cracked · May 2, 2006 · N685CA · Boeing 7272S7 · Fuselage Miscellaneous Structure
  > RIGHT W/W STA 870 AT KEEL BEAM VERTICAL STIFFENER CRACKED AT LOWER END. REMOVED AND REPLACED VERTICAL STIFFENER RIGHT W/W BS 870 P/N 65-18636-378 PO 6206100 IAW B727 SRM 51-30-2.
- [SDR C1HA200685007](https://openairdocs.org/sdr/C1HA200685007.md): Floorbeam · corroded · May 2, 2006 · N685CA · Boeing 7272S7 · Fuselage Main, Floor Beam
  > CABIN CORROSION FLOORBEAM 344 LBL 48 TO RBL 12. FOUND CORROSION OUT OF LIMIT IAW B727 SRM 53-10-1. REMOVED DAMAGED AREA, FABBED UPPER CHORD FROM BAC 1505-29221 ANGLE FROM BAC 149-2831 IAW B727 SRM 53-10-2 FIG 7, ALODINE & PRIME IAW B727 SRM 51-10-2, INSTALLE
- [SDR C1HA200685006](https://openairdocs.org/sdr/C1HA200685006.md): Angle · cracked · May 2, 2006 · N685CA · Boeing 7272S7 · Trailing Edge Flaps
  > RT WING I/B MID FLAP HAS CRACK AT EDGE OF CUTOUT BELOW THE I/B MECHANISM. CUT OUT DAMAGED SECTION OF CHORD (70 INCHES) IN LENGTH, FABRICATED NEW SECTION P/N BAC 1503 100046 (70 INCHES) & SPLICE ANGLE 7075 T6.050 IAW B727 SRM 57-50-2 FIG 5 & 51-40-4 FIG 1, TR
- [SDR C1HA200685008](https://openairdocs.org/sdr/C1HA200685008.md): Seat Track · corroded · May 2, 2006 · N685CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN SEAT TRACK AT LBL 45 DEEP CORROSSION INSIDE CROWN AREA AT STA 950 TO 970. CUT OUT SEAT TRACK FROM STA 950 TO 1115 IAW B727 SRM 53-10-1 FIG 3. FAB NEW SEAT TRACK FROM BAC1520-797 7075 T6.02 IAW B727 SRM 53-10-5. ALODINE & PRIMED IAW B727 SRM 51-
- [SDR C1HA200685005](https://openairdocs.org/sdr/C1HA200685005.md): Seat Track · corroded · May 2, 2006 · N685CA · Boeing 7272S7 · Fuselage, Seat/Cargo Attach Fittings
  > UPPER CABIN SEAT TRACK HAS CORROSION STA 469 RBL 45. FOUND CORROSION OUT OF LIMITS. REMOVED SEAT TRACK RBL 400 TO 480 IAW B727 SRM 51-30-2, FABRICATED NEW SEAT TRACK FROM BAC 1520 KTP 017 792 7178 IAW B727 SRM 53-10-2 FIG 7, & 51-20-1. ALODINED & PRIMED IAW

Next page: https://openairdocs.org/model/boeing-727-2s7/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 aircraft_model_key = '7272S7'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-2s7/reports

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