# Service difficulty reports: Boeing 727-180C

A list on [Boeing 727-180C](https://openairdocs.org/model/boeing-727-180c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 6 · 279 reports

- [SDR UPS06248626](https://openairdocs.org/sdr/UPS06248626.md): Indicator · inoperative · Nov 14, 2006 · N920UP · Boeing 727180C · Fuel Quantity Indicator
  > N/A ATB - FUEL IMBALANCE BETWEEN TANK NR 1 AND NR 3 STARTED AT NR 1, 11.9, NR 3, 11.2 AFTER TA/O TANK NR 1, 11.5, TANK NR 3, 9.5 DEFERRED NR 3 COCKPIT GAUGE NR M337674 ISSUED. DEFERRED NR 3 COCKPIT GAUGE IAW MEL 28-11-1-1. VERIFIED FUELING STATION GAUGES ARE O
- [SDR UPS06248464](https://openairdocs.org/sdr/UPS06248464.md): Light · weak · Nov 2, 2006 · N920UP · Boeing 727180C · Emergency Lighting
  > FOUND COCKPIT EMERGENCY EXIT LIGHT WEAK. REPLACED C/P EMERGENCY LIGHT ASSY CKS OK.
- [SDR UPS06247335](https://openairdocs.org/sdr/UPS06247335.md): Smoke Goggles · dirty · Jul 15, 2006 · N920UP · Boeing 727180C · Emergency Equipment
  > F/O SMOKE GOGGLES DIRTY AND NOT BAGGED. INSTALLED NEW MASK.
- [SDR UPS06246958](https://openairdocs.org/sdr/UPS06246958.md): Skin · corroded · May 12, 2006 · N920UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:SV RIVET HEAD POPPED OFF AT STA 680 LONG 6L JUST FWD OF DOUBLER. FOUND CORROSION IN LAP FROM STA 620-720 AT S-6L. REPAIRED LAP PER EO B727-5330-0509-T APPX C, SAA EA 727-5330-01-A0201, AND EO B727- 5330-24413-A.
- [SDR UPS06246273](https://openairdocs.org/sdr/UPS06246273.md): Panel · delaminated · Feb 24, 2006 · N920UP · Boeing 727180C · Spoilers
  > INSPECTION TYPE:N/A RT INBOARD SPOILER PANEL DELAMINATED. REPAIRED SPOILER PANEL PER SRM 51-40-21.
- [SDR UPS05245867](https://openairdocs.org/sdr/UPS05245867.md): Light · loose · Dec 9, 2005 · N920UP · Boeing 727180C · Emergency Lighting
  > COCKPIT EMERGENCY EXIT LIGHT LOOSE OUT OF FITTING ABOVE DOOR. SECURED EMERGENCY EXIT LIGHT ON CASE AND INSTALLED LENS REF MM 33-50-67-2.
- [SDR UPS05245632](https://openairdocs.org/sdr/UPS05245632.md): Fitting · cracked · Oct 4, 2005 · N920UP · Boeing 727180C · Wing, Landing Gear Attach Fittings
  > INSPECTION TYPE: C, SEVERAL CRACKS ON LT MLG TRUNNION FITTING. REPLACED MLG TRUNNION FITTING IAW AAAE EO = 2005-091-001 AND UPS FILE APPROVAL B727-5740-23096.
- [SDR UPS03240426](https://openairdocs.org/sdr/UPS03240426.md): Longeron · cracked · Apr 10, 2003 · N920UP · Boeing 727180C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C2, WHILE WORKING EO B727-5330-17160-A, STA 366.65 LONGERON S1 IS CRACKED. REMOVED FASTENERS, CUTOUT DAMAGE, NDT VERIFIED NO CRACKS AT CUTOUT. FABRICATED AND INSTALLED REPAIR CHANNEL AND FILLER IAW SRM 53-10-2 FIG 9 AND 53-10-3 FIG 2.
- [SDR UPS03240405](https://openairdocs.org/sdr/UPS03240405.md): Light · inoperative · Apr 2, 2003 · N920UP · Boeing 727180C · Engine Starting System
  > AT CRUISE NR 1 START VALVE LIGHT FLICKERED THEN CAME ON FOR A FEW SECONDS. ENG BLEED WAS CLOSED AND ENGINE SHUTDOWN IN ACCORDANCE WITH AOM PROCEDURES. REMOVED AND REPLACED NR 1 ENGINE START VALVE IAW TAY ENGINE MM 80-11-01. OPS CHECK NORMAL.
- [SDR UPS03240223](https://openairdocs.org/sdr/UPS03240223.md): Light · inoperative · Feb 22, 2003 · N920UP · Boeing 727180C · Emergency Lighting
  > EMERGENCY EXIT LIGHT AT CREW ENTRANCE DOOR INOP. RESET LIGHT PACK, CHECKS GOOD.
- [SDR UPS03240209](https://openairdocs.org/sdr/UPS03240209.md): Battery · inoperative · Feb 19, 2003 · N920UP · Boeing 727180C · Emergency Lighting
  > INSPECTION TYPE: C, COCKPIT EMERGENCY EXIT LIGHT INOPERATIVE. REPLACED BATTERIES AND OPS CHECKS GOOD IAW M/M 33-50-01.
- [SDR UPS02239825](https://openairdocs.org/sdr/UPS02239825.md): Light · not seated · Oct 25, 2002 · N921UP · Boeing 727180C · Emergency Lighting
  > INSPECTION TYPE:PFLT EMERGENCY EXIT LIGHTS ABOVE CABIN ENTRY DOOR ARE VERY DIM. CHARGED BATTERY FOR 3 HRS, RESEATED LIGHT ASSY, GROUND CHECK GOOD.
- [SDR UPS02239750](https://openairdocs.org/sdr/UPS02239750.md): Light · inoperative · Oct 15, 2002 · N921UP · Boeing 727180C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS INOPERATIVE. REPLACED CREW ENTRY DOOR EMERGENCY EXIT LIGHT ASSY. OPS CHECK GOOD MM 33-50-01.
- [SDR UPS02238111](https://openairdocs.org/sdr/UPS02238111.md): Skin · corroded · Apr 22, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C CORROSION FOUND AT LAP SKINS BS 479 STRINGER 26R FASTENERS REMOVED IAW SRM51-30-02, UPUPER SKIN CUT OUT BETWEEN BS 47 2-485, NDT NDF, REPAIR PARTS FABRICATED IAW AND INSATLLED IAW EO B72 7-5330-16775.
- [SDR UPS02238094](https://openairdocs.org/sdr/UPS02238094.md): Skin · cracked · Apr 22, 2002 · N921UP · Boeing 727180C · Leading Edge Devices
  > INSPECTION TYPE:C NR 3 KRUEGER FLAP ANTI ICE SKIN CRACKED 14 INCHES FROM I/B END. INSPECTED IAW NDTM PT 6 51-00-00 FIG 4, REPAIR CARRIED OUT IAW UPS EO B727-5750-3082-D.
- [SDR UPS02238102](https://openairdocs.org/sdr/UPS02238102.md): Seat Track · corroded · Apr 20, 2002 · N921UP · Boeing 727180C · Fuselage Main, Structure
  > INSPECTION TYPE:C CORROSION FOUND ON SEAT TRACK O/B FLANGE AT BS 500 AT R/H O/B SEAT T RACK SEAT TRACK REPAIRED IAW SRM 53-10-5
- [SDR UPS02238068](https://openairdocs.org/sdr/UPS02238068.md): Doubler · corroded · Apr 18, 2002 · N920UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C DOUBLER ON LEFT FWD WHEEL WELL PANEL IS PULLING LOOSE, AND IS CORRODED AT LOWER FASTENER. REMOVED AND REPLACED DOUBLER PER B727 SRM 51-30-2 ON LEFT FWD WHEEL WELL BELOW APU EXTINGUISHER BLOW OUT DISC.
- [SDR UPS02238112](https://openairdocs.org/sdr/UPS02238112.md): Doubler · corroded · Apr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION BETWEEN FUSELAGE SKIN AND TOILET SERVICE PAN UPPER FLANGE, AFT SERVICE PAN. AREA PAINT STRIPPED, SERVICE PAN DE-RIVETED AND REMOVED, SKIN PANEL DE-RIVETED BETWEEN STR 17L-23L BS 1183 - 1150. INTERNAL DOUBLER AROUND PAN FO
- [SDR UPS02238103](https://openairdocs.org/sdr/UPS02238103.md): Skin · cracked · Apr 18, 2002 · N921UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CRACK IN FUSELAGE SKIN BS 310 S8 L/H AT FWD ENTRY DOOR FWD D OOR CUT OUT REPAIR CARRIED OUT IAW UPS EO B727-5340-1460
- [SDR UPS01237092](https://openairdocs.org/sdr/UPS01237092.md): Hydraulic Line · cracked · Oct 18, 2001 · N920UP · Boeing 727180C · Hydraulic System, Main
  > INSPECTION TYPE:N/A SYSTEM A-HYDRAULIC FAILURE, QTY ZERO. FOUND NR 13 SPOILER ACTUATOR RETURN LINE CRACKED. PER GMM INSTALLED A FLEX HOSE. CHECKED CASE DRAIN FILTERS, REPLACED NR 2 HYD EDP. SERVICED SYSTEM AND OPS CHK'D GOOD. PUMPED CHANGED DUE TO BYPASS S
- [SDR UPS01235994](https://openairdocs.org/sdr/UPS01235994.md): Light · inoperative · May 24, 2001 · N920UP · Boeing 727180C · Emergency Lighting
  > INSPECTION TYPE:N/A REF ITEM 1 THIS PAGE. SUSPECT EMER LIGHT FWD SOCKET TO BE BAD. REMOVED AND REPLACED EMERGENCY EXIT LIGHT, OPS CK GOOD.
- [SDR UPS01235993](https://openairdocs.org/sdr/UPS01235993.md): Light · malfunctioned · May 24, 2001 · N920UP · Boeing 727180C · Emergency Lighting
  > INSPECTION TYPE:N/A EMERGENCY EXIT LIGHT CAME ON IN FLIGHT, NOW WILL NOT TEST ON THE GROUND. PERFORMED OPS CHECK OF EMERGENCY EXIT LIGHTS, OPS CHECK OK. NO DEFECTS NOTED.
- [SDR UPS01235238](https://openairdocs.org/sdr/UPS01235238.md): Cover · loose · Mar 7, 2001 · N920UP · Boeing 727180C · Emergency Lighting
  > INSPECTION TYPE:N/A, COCKPIT EMERGENCY EXIT LIGHT COVER FALLS OFF ON LANDING. REPLACED EXIT LIGHT COVER.
- [SDR UPS01234998](https://openairdocs.org/sdr/UPS01234998.md): Fitting · broken · Feb 15, 2001 · N921UP · Boeing 727180C · Crew Oxygen System
  > INSPECTION TYPE:IN OXYGEN BOTTLE ATTACHING HARDWARE BROKEN. *S/D* REMOVED AND REPLACED MS FITTING ON BLOWOUT LINE AND UPPER 02 BOTTLE CLAMP. REMOVED AND REPLACED 02 BOTTLE. LK CHECK GOOD.
- [SDR UPS01234918](https://openairdocs.org/sdr/UPS01234918.md): Access Panel · corroded · Jan 26, 2001 · N920UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:IN FUSELAGE - RT ACCESS PANEL 3420 - BS 630 AFT FRAME OF ACCESS PANEL CUTOUT HAS CORROSION BEYOND LIMITS PER B727 SRM 53-01-1. REMOVED CENTER SECTION OF AFT FRAME OF PANEL CUTOUT ON FUSELAGE BODY PANEL 3420 AT BS 630, FABRICATED A NEW SECTION
- [SDR UPS01234919](https://openairdocs.org/sdr/UPS01234919.md): Angle · cracked · Jan 25, 2001 · N920UP · Boeing 727180C · Wing Miscellaneous Structure
  > INSPECTION TYPE:IN RT WING LEADING EDGE STA 349.6 WEB O/B UPPER SUPPORT ANGLE CRACKED. STOPPED DRILLED CRACK PER B727 SRM 51-10-1, NDT STOPPED DRILLED INSTALLED ANGLE REPAIR PER B727 SRM 51-40-3.
- [SDR UPS00234545](https://openairdocs.org/sdr/UPS00234545.md): Switch · inoperative · Dec 13, 2000 · N921UP · Boeing 727180C · Crew Oxygen System
  > INSPECTION TYPE:N/A CO PILOTS EMERG 0XYGEN SWITCH FAILS TO FULLY CLOSE ***SUPPLEMENTAL MRR*** REPLACED CO-PILOTS REGULATION W/SERVICABLE RUGULATION AND REPLACED W ITH SERVICABLE BOTTLE. LEAKED CHECK OK OPS CHECK PER 727 MM CHPT 35- 11-31 AND 12-15-11
- [SDR UPS00234250](https://openairdocs.org/sdr/UPS00234250.md): Motor · failed · Oct 26, 2000 · N921UP · Boeing 727180C · Trailing Edge Flap Control System
  > INSPECTION TYPE:C, O/B ALT FLAP MOTOR NOT RETRACTING FLAPS. REPLACED MOTOR IAW MM 27-51-141.
- [SDR UPS00234247](https://openairdocs.org/sdr/UPS00234247.md): Shear Tie · cracked · Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, Structure
  > INSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 318 AND LBL 4. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS00234246](https://openairdocs.org/sdr/UPS00234246.md): Shear Tie · cracked · Oct 18, 2000 · N921UP · Boeing 727180C · Fuselage Main, Structure
  > INSPECTION TYPE:C, FLOORBEAM SHEAR TIE CRACKED AT BS 312 RBL 24. REPAIR CARRIED OUT IAW SRM 51-40-2.
- [SDR UPS00234257](https://openairdocs.org/sdr/UPS00234257.md): Flange · cracked · Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, SUSPECT CRACK ON AFT O/B AND FWD FLANGES OF BS 930 FUSELAGE FITTING BETWEEN S18A AND S19 LT. REPAIR CARRIED OUT IAW UPS EO B727-5310-2611 APPENDIX 8.1
- [SDR UPS00234249](https://openairdocs.org/sdr/UPS00234249.md): Fitting · corroded · Oct 16, 2000 · N921UP · Boeing 727180C · Fuselage Main, Attach Fittings
  > INSPECTION TYPE:C, DUE TO EXCESSIVE CORROSION IN BS 940 LT FITTING FASTENER HOLES, REPLACE FITTING BS 940 LT. REPLACED IAW UPS EO B727-5310-4501 APPENDIX C.
- [SDR UPS00234256](https://openairdocs.org/sdr/UPS00234256.md): Stiffener · cracked · Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. REPAIR CARRIED OUT IAW SRM 51-30-2 DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.
- [SDR UPS00234255](https://openairdocs.org/sdr/UPS00234255.md): Stiffener · cracked · Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORIZ STIFFENER AT BS 900 APPROX IS CRACK ED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. REPAIR CARRIED OUT IAW DRG NR 65-28900 AND SMRO EO 2000-38-006 UPS ENGINEERING FILE NR 727-53-2293.
- [SDR UPS00234252](https://openairdocs.org/sdr/UPS00234252.md): Stiffener · cracked · Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, KEEL BEAM AREA, HORIZ STIFFENER AT BS 900 IS CRACKED. STIFFENER IS LOCATED ON INTERNAL SIDE OF LT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG NR 65-18636 AND SRM 51-30-2.
- [SDR UPS00234251](https://openairdocs.org/sdr/UPS00234251.md): Stiffener · cracked · Oct 14, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, KEEL BEAM AREA (INTERNAL) HORZ STIFFENER AT BS 900 APPROX IS CRACKED AT SITE OF PREVIOUS REPAIR RT KEEL BEAM WALL. STIFFENER INSTALLED IAW DRG 65-18636 AND SRM 51-30-2.
- [SDR UPS00234248](https://openairdocs.org/sdr/UPS00234248.md): Mount · corroded · Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount Section
  > INSPECTION TYPE:C, ENGINE NR 3 FWD MOUNT PITTING CORROSION FWD IN BOTH I/B MOUNT HOLES. REPAIR CARRIED OUT IAW EO B7274401592.
- [SDR UPS00234244](https://openairdocs.org/sdr/UPS00234244.md): Mount · corroded · Oct 13, 2000 · N921UP · Boeing 727180C · Engine Mount Section
  > INSPECTION TYPE:C, ENG NR 1 FWD MOUNT, PITTING CORROSION FOUND IN FWD BOLT HOLES I/B, O/B. REPAIR CARRIED OUT IAW EOJ NR B727-5440-11592.
- [SDR UPS00234241](https://openairdocs.org/sdr/UPS00234241.md): Beam · cracked · Oct 13, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CRACK FOUND AT BS 1183 BULKHEAD VERTICAL BEAM RBL 26.83 AT WL 259.5. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631.
- [SDR UPS00234254](https://openairdocs.org/sdr/UPS00234254.md): Flange · corroded · Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, EVIDENCE OF CORROSION TO S18A FLANGE (HORIZ) AT BS 870 LT. REPAIR CARRIED OUT IAW SRM 53-10-1 AND 51-30-2 AND SMRO EO 2000-38-003 AND EO B727-5330-3815 UPS ENGINEERING FILE NR 727-53-2292.
- [SDR UPS00234243](https://openairdocs.org/sdr/UPS00234243.md): Skin · cracked · Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SKIN CRACKS AT BS 203.8 RT AT WL 18 AND WL 20. DAMAGE REPAIRED IAW SRM 53-30-3 FIG 3.
- [SDR UPS00234242](https://openairdocs.org/sdr/UPS00234242.md): Bracket · cracked · Oct 12, 2000 · N921UP · Boeing 727180C · Engine Thrust Reverser
  > INSPECTION TYPE:C, ENGINE NR 3 THRUST REV O/B FAIRING MID SUPPORT BRACKET CRACKED. BRACKET REPLACE IAW MM 20-80-01.
- [SDR UPS00234240](https://openairdocs.org/sdr/UPS00234240.md): Beam · cracked · Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, FOUR CRACKS FOUND AT BS 1183 BULKHEAD VERTICAL BEAM LBL 26.83 AT WL 257 AND WL 260. REPAIR CARRIED OUT IAW APPENDIX D OF EO B727-5311-0631AND BOEING DRG 65C34406.
- [SDR UPS00234228](https://openairdocs.org/sdr/UPS00234228.md): Skin · cracked · Oct 12, 2000 · N921UP · Boeing 727180C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C, SKIN CRACK AT BS 243.7 WL 19 LT. CRACKED AREA OF SKIN CUT OUT IAW SRM 53-30-3 FIG 3. HFEC C/O IN ALL ACCESSED HOLES AND AROUND PERIFERY OF CUTOUT. POST FASTENER REMOVAL AND SKIN CUTOUT IAW B727 NDTM. NO DEFECTS FOUND IN FASTENER HOLES AN
- [SDR UPS00234229](https://openairdocs.org/sdr/UPS00234229.md): Structure · corroded · Oct 11, 2000 · N921UP · Boeing 727180C · Fuselage Main, Structure
  > INSPECTION TYPE:C, BILGE IN SKIN (SUSPECT CORROSION) AT BS 1030 ABOVE STR 18 LT. GILL LINER REMOVED IAW MM 25-52-02. CORROSION ON EXTRUSION FOUND TO BE CORRODED AND OUTSIDE LIMITS SRM 53-30-01. NEW EXTRUSION INSTALLED IAW SRM 51-30-02. GILL LINER INSTALLED
- [SDR UPS00233068](https://openairdocs.org/sdr/UPS00233068.md): Floor Support · cracked · Jun 23, 2000 · N921UP · Boeing 727180C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE: C CARGO BAY FLOOR SUPPORT LONGTITUDINAL BEAMS CRACKED TWO PLACES, BS 2020, BL 0, BS 1988, LBL 30 FLOOR SUPPORT BEAMS REPAIRED IAW SRM 53-10-07
- [SDR UPS99231117](https://openairdocs.org/sdr/UPS99231117.md): Link · corroded · Nov 8, 1999 · N921UP · Boeing 727180C · Main Landing Gear Attach Section
  > INSPECTION TYPE: AD, RT MLG TRUNNION LINK HAS PITTING CORROSION ON FORWARD BEARING SURFACE. REPLACED TRUNNION LINK ASSEMBLY. INSTALLED IAW MM 32-11-01.
- [SDR UPS99231116](https://openairdocs.org/sdr/UPS99231116.md): Support · corroded · Nov 8, 1999 · N921UP · Boeing 727180C · Trailing Edge Flaps
  > INSPECTION TYPE: AD, RT SUPPORT ASSEMBLY INBOARD FLAP TRACK FORWARD CORRODED. SUPPORT ASSEMBLY REPLACED IAW BOEING DRAWING NR 65 19297, SHEET 3, REV E.
- [SDR UPS99231120](https://openairdocs.org/sdr/UPS99231120.md): Fitting · leaking · Nov 5, 1999 · N921UP · Boeing 727180C · Fuel Storage
  > INSPECTION TYPE:AD, FUEL LEAK AT RT WING BEHIND LANDING GEAR TRUNNION FITTING, ONLY STAINS. THIS MRR RESUBMITTED TO INCLUDE TRUNNION FITTING, FUEL LEAK REPAIRED IAW SMRO EO 99-35-001. TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.
- [SDR UPS99231119](https://openairdocs.org/sdr/UPS99231119.md): Fitting · leaking · Nov 5, 1999 · N921UP · Boeing 727180C · Fuel Storage
  > INSPECTION TYPE:AD FUEL LEAK AT LT WING BEHIND LANDING GEAR TRUNNION FITTING. THIS MRR RESUBMIT TO INCLUDE TRUNNION FUEL LEAK. REPAIRED IAW SMRO EO 99-35-01 TRUNNION FITTING REMOVED AND REPLACED DUE TO MECHANICAL DAMAGE.

Next page: https://openairdocs.org/model/boeing-727-180c/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 = '727180C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-180c/reports

---
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