# Service difficulty reports: Boeing 727-30C

A list on [Boeing 727-30C](https://openairdocs.org/model/boeing-727-30c.md).

Newest first. General aviation reporting is voluntary.

Page 1 of 19 · 931 reports

- [SDR UPS07248886](https://openairdocs.org/sdr/UPS07248886.md): Slide · dislodged · Jan 19, 2007 · N919UP · Boeing 72730C · Escape Slide
  > FWD ENTRY ESCAPE SLIDE IS OUT OF CONTAINER. INSTALLED FORWARD ENTRY DOOR EVACUATION SLIDE IAW 25-60-14-2. OPS CHECK GOOD.
- [SDR UPS06248684](https://openairdocs.org/sdr/UPS06248684.md): Skin · cracked · Nov 14, 2006 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > 3 INCH CRACK ON FUSELAGE SKIN AT 10 O'CLOCK POSITION RUNNING FWD AND AFT AT STA 348.2, BETWEEN STRINGERS 5L & 6L. ADDITIONAL DISBONDING APPROXIMATELY 4 X 4 INCHES. C/W EO B727-5330-25585A TO FERRY A/C TO BFM 9014 D337794 ISSUED.
- [SDR UPS06248513](https://openairdocs.org/sdr/UPS06248513.md): Slide · dislodged · Nov 7, 2006 · N919UP · Boeing 72730C · Escape Slide
  > FOUND DOOR SLIDE ON FLOOR. RE-INSTALLED ESCAPE SLIDE PER 25-60-14-2.
- [SDR UPS06248330](https://openairdocs.org/sdr/UPS06248330.md): Battery · inoperative · Oct 26, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHTS ABOVE THE MAIN ENTRY DOOR AND ABOVE THE COCKPIT ENTRY DOOR ARE INOP. REMOVED AND REPLACED EMERGENCY EXIT LIGHT ASSY ON MAIN ENTRY DOOR PER MM 33-50-90-2. REMOVED AND REPLACED BATTERIES ON COCKPIT ENTRY DOOR. OPS CHECK GOOD.
- [SDR UPS06247834](https://openairdocs.org/sdr/UPS06247834.md): Light · no test · Aug 29, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS WILL NOT TEST. REMOVED AND REPLACED C/P PORTABLE EMERGENCY LIGHT ASSY IAW MM 33-50-67-2. SYS OPS CKS OK.
- [SDR UPS06247827](https://openairdocs.org/sdr/UPS06247827.md): Slide · dislodged · Aug 28, 2006 · N919UP · Boeing 72730C · Escape Slide
  > INSPECTION TYPE: NA ESCAPE SLIDE FELL OUT OF CASE ON MAIN ENTRY DOOR REPLACED ENTRY DOOR EVACUATION SLIDE IAW MM 25-60-14-2.
- [SDR UPS06247826](https://openairdocs.org/sdr/UPS06247826.md): Lamp · failed · Aug 28, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE:NA EMERGENCY LIGHT ABOVE CREW ENTRY DOOR DIM, RELAMPED. OPS CK NORMAL IAW 25 60 00.
- [SDR UPS06247717](https://openairdocs.org/sdr/UPS06247717.md): Battery · inoperative · Aug 17, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > INSPECTION TYPE: N/A EMERGENCY EXIT LIGHTS DO NOT ILLUMINATE WITH SWITCH ON. REMOVED AND REPLACED EMERGENCY LIGHT BATTERIES. OPS CK NORMAL.
- [SDR UPS06247529](https://openairdocs.org/sdr/UPS06247529.md): Battery · discharged · Jul 31, 2006 · N919UP · Boeing 72730C · Emergency Lighting
  > FOUND COCKPIT DOOR EMERGENCY EXIT LIGHT INOP. REPLACED BATTERIES AS REQUIRED.
- [SDR UPS06246808](https://openairdocs.org/sdr/UPS06246808.md): Fairing · delaminated · May 8, 2006 · N919UP · Boeing 72730C · Aerodynamic Fairings
  > DELAM ON L/AFT WING TO BODY FAIRING PANEL NR 3510 JUST AFT OF HYD SYS BAY REF EO B727-5350-24306. PERFORMED INTERIM REPAIR PER EO B727-5350-24306 STEP 6. DEFERRED FOR REPEAT INSPECTION EVERY 30 DAYS AND PERM BY C-CK. NR D 325051 ASSIGNED INSTALLATION OF PAN
- [SDR UPS06246793](https://openairdocs.org/sdr/UPS06246793.md): Light · inoperative · May 4, 2006 · N918UP · Boeing 72730C · Emergency Lighting
  > EMERGENCY EXIT LIGHT CAME OUT OF SOCKET. REINSTALLED ASSEMBLY. OPS CK GOOD PER AMM 33-50-01-5.
- [SDR 2006FA0000645](https://openairdocs.org/sdr/2006FA0000645.md): Control Valve · failed · Nov 8, 2005 · N918UP · Boeing 72730C · Extinguishing System
  > NR 2 ENGINE FIRE EXTINGUISHING SELECTOR CONTROL VALVE FAILED TO OPEN DURING ROUTINE TESTING IAW UPS ROUTINE TASK CARD TC 2-221-12. THE VALVE SOLENOID HOUSING WAS NOTED AS BEING CORRODED. (K)
- [SDR UPS05245823](https://openairdocs.org/sdr/UPS05245823.md): Stringer · corroded · Nov 1, 2005 · N918UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE:C STRINGER 24 RT FOUND CORRODED AT BS 725. PLEASE INVESTIGATE DAMAGE FOUND TO BE BEYOND LIMITS IAW SRM 53-10-3. DAMAGED SECTION OF STRINGER 24R CUT OUT AND REMOVED. AREA REPAIRED IAW 53-10-3 FIG 1 DETAIL 1 PAGE 4B.
- [SDR UPS05245859](https://openairdocs.org/sdr/UPS05245859.md): Skin · cracked · Oct 25, 2005 · N918UP · Boeing 72730C · Cargo/Baggage Doors
  > INSPECTION TYPE:C AFT CARGO DOOR CRACK ON INNER SKIN SECOND INSPECTION HOLE FWD EDGE AT BOTTOM. REMOVE FASTENER AND CHECK DEPTH OF CRACK TO DETERMINE REPAIR. HFEC CARRIED OUT AND CRACK FOUND CONTAINED WITHIN FASTENER HOLE. REPAIRED IAW SRM 51-40-02.
- [SDR UPS05245826](https://openairdocs.org/sdr/UPS05245826.md): Intercostal · cracked · Oct 24, 2005 · N918UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C STA 660, ST 29R REPAIR TO INTERCOSTAL IS CRACKED. PLEASE REPAIR IAW SRM. REPAIR BRACKET FABRICATED IAW SRM 51-20-071 FIG 7. REPAIR BRACKET REPLACED IAW SRM 51-30-02.
- [SDR UPS05245861](https://openairdocs.org/sdr/UPS05245861.md): Link · cracked · Oct 18, 2005 · N918UP · Boeing 72730C · Main Landing Gear
  > INSPECTION TYPE:C RT MLG UPLOCK FWD SUPPORT LINKS CRACKED. REPLACE LINKS. RT MLG UPLOCK FWD SUPPORT LINKS REPLACED IAW MM 20-80-01.
- [SDR UPS05245851](https://openairdocs.org/sdr/UPS05245851.md): Spar · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Wing Spar
  > AREA OF SUSPECT CORROSION ON WING CENTER SECTION REAR SPAR LWR CHORD BS 870 RBL36 DUE TO 2 POPPED FASTENER HEADS. PLEASE INVESTIGATE AND RECTIFY AS NECESSARY. AS PER BOEING INSTRUCTIONS THE LWR CHORD WAS REPLACED. NEW CHORD WAS CUT AT RBL 9.5. REPAIR SPLICE
- [SDR UPS05245832](https://openairdocs.org/sdr/UPS05245832.md): Skin · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > EVIDENCE OF CORROSION AT BS 360 STR 22L AT FWD END OF STR AT AFT FACE OF FRAME. PLEASE INVESTIGATE AND RECTIFY. CORROSION BLENDED OUT IAW SRM 51-10-06. CORROSION FOUND TO BE OUTSIDE LIMITS IAW SRM 51-10-1. REPAIR STRAP FABRICATED IAW SRM 51-20-1 FIG 7. M
- [SDR UPS05245821](https://openairdocs.org/sdr/UPS05245821.md): Skin · corroded · Oct 16, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NDT INSPECTION HAS INDICATION OF MATERIAL LOSS AT BS 441 FWD OF CENTER LINE AT STR 8L, INVESTIGATE. CORROSION FOUND BETWEEN SKIN AND DOUBLER. CORROSION REMOVED AND FOUND BE WITHIN LIMITS, AREA REPROTECTED IAW SRM 51-30-02.
- [SDR UPS05245836](https://openairdocs.org/sdr/UPS05245836.md): Trunnion · cracked · Oct 15, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > RT TRUNNION ATTACH FITTING HAS CRACK AT OB FLANGE HOLE E RUNNING UP APPROX 2.5 INCHES. REMOVE AND REPLACE FITTING. RT TRUNNION FITTING FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. REPLACED IAW UPS AUTHORIZATION B727-5740-23046-B.
- [SDR UPS05245831](https://openairdocs.org/sdr/UPS05245831.md): Skin · corroded · Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > SURFACE CORROSION ON LAP JOINT BETWEEN S-4L AND 5L AT LOCATIONS BETWEEN BS 852 AND 1011. CORROSION REMOVED IAW SRM 51-10-2 (.002") AND FOUND WITHIN LIMITS IAW SRM 51-20-4.
- [SDR UPS05245824](https://openairdocs.org/sdr/UPS05245824.md): Support · corroded · Oct 14, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > INSPECTION TYPE:C RT MLG TRUNNION BUTTERFLY FITTING HAS CORROSION. PLS REPLACE. SUPPORT REPLACED IAW DRW 65-19296.
- [SDR UPS05245860](https://openairdocs.org/sdr/UPS05245860.md): Bushing · cracked · Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 3 AFT MOUNT FITTING HAS CORROSION ON INNER SURFACE OF UPPER USHING. REPLACE BUSHING. REPLACED BUSHING IAW OHM 20-50-03.
- [SDR UPS05245827](https://openairdocs.org/sdr/UPS05245827.md): Mount · corroded · Oct 13, 2005 · N918UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE:C ENGINE NR 3 FWD MOUNT FITTING HAS PITTING CORROSION ON BOTH OUTBOARD HOLES. REPAIR. REPAIRED IAW EO B727-5540-11592-A.
- [SDR UPS05245833](https://openairdocs.org/sdr/UPS05245833.md): Skin · corroded · Oct 12, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > AREA OF SUSPECT CORROSION ON CROWN SKIN BS 521 TO BS 515 BETWEEN STR 2L AND 3L. PLEASE PAINT STRIP AREA, REMOVE FASTENERS IF REQUIRED, REINSPECT AND RECTIFY AS NECESSARY. REPAIRED IAW UPS AUTHORIZATION B727-5330-23323-A
- [SDR UPS05245822](https://openairdocs.org/sdr/UPS05245822.md): Support Fitting · cracked · Oct 12, 2005 · N918UP · Boeing 72730C · Wing, Attach Fittings
  > RT WING FRONT SPAR TO BODY FITTING HAS SUSPECT CRACK ON OUTBD SIDE OF BOTTLE PIN. FITTING REPLACED IAW DWG 65C13724 AND UPS EO B727-5310-7477.
- [SDR UPS05245835](https://openairdocs.org/sdr/UPS05245835.md): Trunnion · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage, Landing Gear Attach Fittings
  > LT MLG SUPPORT FITTING HAS CRACK INDICATION IN HOLE B & C ON INB FLANGE AND HOLES E IN COUNTERSINKS. REPAIR AND REPLACE FITTING LT MLG TRUNNION REMOVED AND FOUND CRACKED OUTSIDE REPAIRABLE LIMITS IN UPS EO B727-5740-20666C. TRUNNION REPAIRED IAW UPS AUTHORIZ
- [SDR UPS05245829](https://openairdocs.org/sdr/UPS05245829.md): Skin · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C NDT INDICATES 2 CRACKS EMINATING FROM FASTENERS " BS235.8 STR16L-17L. PLEASE REPAIR IAW SRM 53-30-3 FIG 3. FASTENERS REMOVED FROM AFFECTED AREA IAW SRM 51-80-02. AFFECTED AREA CUTOUT IAW SRM 53-30-3. HFEC CARRIED OUT AROUND CUTOUT AND ON
- [SDR UPS05245828](https://openairdocs.org/sdr/UPS05245828.md): Skin · cracked · Oct 11, 2005 · N918UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT SKIN CRACKS AT UPPER FWD CORNER OF FWD ENTRY DOOR CUT OUT BETWEEN STR 7L AND 8L. PLEASE CARRY OUT NDI AND RECTIFY AS NECESSARY IAW SRM ADDENDUM. HFEC CARRIED OUT IAW NDTM 51-00-00 PT6 FIG 4. TWO CRACKS FOUND. DAMAGE REMOVED IAW EO
- [SDR UPS05245834](https://openairdocs.org/sdr/UPS05245834.md): Skin · cracked · Oct 9, 2005 · N918UP · Boeing 72730C · Service Doors
  > FOUND SKIN CRACK AT FASTENER HOLE IN MID GALLEY DOOR CUT OUT, UPPER FWD CORNER. PLEASE CONFIRM WITH NDI AND RECTIFY AS NECESSARY HFEC CARRIED OUT ON FASTENER HOLES COMMON TO REPAIR IAW 727NDTM 51-00- 00 PT6 FIG 16. THREE CRACKS FOUND. REPAIR CARRIED OUT IAW
- [SDR UPS05245266](https://openairdocs.org/sdr/UPS05245266.md): Skin · corroded · Aug 6, 2005 · N919UP · Boeing 72730C · Vertical Stabilizer, Plate/Skin
  > INSPECTION TYPE: C, NR 2 ENG UPPER HORIZ FIREWALL SURFACE TO VERT FIN, LT, ANGLE HAS EVIDENCE OF CORROSION ON INNER SURFACE OF VERT FIN SKIN BETWEEN STA 1385 AND 1425 APPROX. SKIN REMOVED AND FOUND CORRODED O/S LIMITS, CHORD BETWEEN BS 1384 AND 1484 FOUND COR
- [SDR UPS05245265](https://openairdocs.org/sdr/UPS05245265.md): Stiffener · corroded · Aug 5, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > LT MLG W/W, EVIDENCE OF CORROSION ON BS 870 VERTICAL STIFFENER AND ATTACH CLIP AT LB 145. CEILING AREA. REPAIR CARRIED OUT IAW SRM 51-30-2 & 51-10-2, 51-10-1.
- [SDR UPS05245262](https://openairdocs.org/sdr/UPS05245262.md): Stiffener · corroded · Aug 4, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > RT MLG W/W, EVIDENCE OF CORROSION ON VERTICAL STIFFENER CEILING AREA BS 870 RBL 45. REPAIR CARRIED OUT IAW SRM 51-40-4.
- [SDR UPS05245263](https://openairdocs.org/sdr/UPS05245263.md): Floorbeam · corroded · Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Main, Floor Beam
  > FLOORBEAM TOP CHORD CORROSION OUTSIDE LIMITS BS 328 RBL 12. REPAIR CARRIED OUT IAW SRM 53-10-8 & 51-10-2.
- [SDR UPS05245207](https://openairdocs.org/sdr/UPS05245207.md): Intercostal · corroded · Aug 3, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C, CORROSION ON INTERCOSTAL BS 294.5 - BS 312 LBL 33. INTERCOSTAL REPLACED IAW BOEING DWG 65-17593 AND SRM 51-30-02.
- [SDR UPS05245205](https://openairdocs.org/sdr/UPS05245205.md): Support · corroded · Aug 2, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C FWD LAV PARTITION SUPPORT STRUCTURAL EXTRUSION CORRODED BS 302 - 344 DOOR THRESHOLD AREA. PARTITION SUPPORT STRUCTURE EXTRUSION REPLACED IAW SRM 51-10-2, 51-20- 2 & 51-30-2.
- [SDR UPS05245261](https://openairdocs.org/sdr/UPS05245261.md): Skin · corroded · Aug 1, 2005 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > AREA OF CORROSION ON SKIN BS 355, BETWEEN STR 8 AND 10 LT. PAINT STRIP AREA IF REQUIRED, REMOVE CORROSION AND RECTIFY. REPAIR CARRIED OUT IAW SRM 51-10-1, 53-30-1 MM 25-21-2 AND AAAE EO 200 5-077-001 UPS ENGINEERING FILE NO. B727-5330-22744-A.
- [SDR UPS05245264](https://openairdocs.org/sdr/UPS05245264.md): Attach Angle · corroded · Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Main, Attach Fittings
  > RT SIDE AFT OF BS 294.5 FWD ATTACHMENT ANGLE OF NWW BOX HAS EVIDENCE OF CORROSION. WEB REPAIRED IAW SRM 51-40-2.
- [SDR UPS05245206](https://openairdocs.org/sdr/UPS05245206.md): Web · corroded · Jul 31, 2005 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C RT SIDE AFT OF RT 294.5 FWD ATTACHMENT ANGLE OF NWW BOX AND RT HAS EVIDENCE OF CORROSION. REPAIR CARRIED OUT IAW SRM 51-10-6, 53-10-1 & 51-40-2.
- [SDR UPS05243629](https://openairdocs.org/sdr/UPS05243629.md): Light · inoperative · Jan 6, 2005 · N919UP · Boeing 72730C · Emergency Lighting
  > L1 DOOR EMERGENCY LIGHT INOP. RESEATED BULB, OPS CHECK GOOD.
- [SDR UPS04242069](https://openairdocs.org/sdr/UPS04242069.md): Fitting · cracked · Mar 17, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF STR END FITTING AT BS 360 S17L FOUND STR END FITTING CRACKED & CORRODED. REPLACED STR END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.
- [SDR UPS04242070](https://openairdocs.org/sdr/UPS04242070.md): Fitting · cracked · Mar 12, 2004 · N919UP · Boeing 72730C · Fuselage Miscellaneous Structure
  > INSPECTION TYPE:C ON REMOVAL OF LOWER SKIN BETWEEN BS 259.5 - BS 360 S22 24L STRINGER END FITTING FOUND CRACKED AT BS 360 S22L. REPLACED STRINGER END FITTING IAW SRM 51-30-02 & DRAWING 65-18420.
- [SDR UPS04242058](https://openairdocs.org/sdr/UPS04242058.md): Stringer · corroded · Mar 11, 2004 · N919UP · Boeing 72730C · Fuselage Main, Longeron/Stringer
  > INSPECTION TYPE: C, ON REMOVAL OF FASTENER AT BS 340 APPROX S25R STRINGER FOUND TO BE CORRODED. REPAIR CARRIED OUT IAW SRM 53-10-3.
- [SDR UPS04242073](https://openairdocs.org/sdr/UPS04242073.md): Skin · corroded · Mar 10, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C ON REMOVAL OF SKIN PANEL AT BS 295.5 & BS 360 S19L - 24L UPPER SKIN UNDER FWD ENTRY DOOR FOUND TO BE EXCESSIVELY CORRODED. REPAIR CARRIED OUT IAW SRMO EO 2004-024-002 UPS ENG.
- [SDR UPS04242072](https://openairdocs.org/sdr/UPS04242072.md): Door Frame · corroded · Mar 9, 2004 · N919UP · Boeing 72730C · Landing Gear Doors
  > INSPECTION TYPE:C TAIL SKID DOOR RIGHT LWR FRAME IS CORRODED ON INNER SURFACE. REPLACED TAIL SKID DOOR IAW MM 32-71-61.
- [SDR UPS04242060](https://openairdocs.org/sdr/UPS04242060.md): Cargo Track · cracked · Mar 9, 2004 · N919UP · Boeing 72730C · Fuselage, Seat/Cargo Attach Fittings
  > INSPECTION TYPE: C, LEFT CARGO TRACK RAIL IN AFT CARGO BAY, VERY FWD SECTION TO BS 950 IS CRACKED. REF CPT 2643 FOR FABRICATION OF CARGO TRACK. REPAIRED CARGO TRACK IAW SRM 53-10-5 FIG 8.
- [SDR UPS04242075](https://openairdocs.org/sdr/UPS04242075.md): Support · corroded · Mar 8, 2004 · N919UP · Boeing 72730C · Drag Control Actuator
  > INSPECTION TYPE:C NR 12 SPOILER ACTUATOR SUPPORT CASTING HAS PITTING AND CORROSION UNDERNEATH THE BOLT HEADS. NR 12 SPOILER ACTUATOR SUPPORT CASTING REPLACED IAW MM 27-61-81, 27-61-01.
- [SDR UPS04242059](https://openairdocs.org/sdr/UPS04242059.md): Mount · corroded · Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE: C, ENGINE NR 1 PYLON FWD MOUNT FITTING, BOTH FWD AFT LARGE AND AFT SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX A.
- [SDR UPS04242057](https://openairdocs.org/sdr/UPS04242057.md): Mount · corroded · Mar 5, 2004 · N919UP · Boeing 72730C · Engine Mount Section
  > INSPECTION TYPE: C, ENGINE NR 3 PYLON FWD MOUNT FITTING, BOTH FWD AND AFT LARGE AND FWD SMALL HOLES HAVE PITTING CORROSION. REPAIR CARRIED OUT IAW EO B727-5440-11592-A APPENDIX B.
- [SDR UPS04242056](https://openairdocs.org/sdr/UPS04242056.md): Skin · bulged · Mar 4, 2004 · N919UP · Boeing 72730C · Fuselage Main, Plate/Skin
  > INSPECTION TYPE:C SUSPECT CORROSION (SKIN BULGING) BETWEEN SKIN & FRAME AT BS 260 FROM STR 18L - S19L. REF N/R 740347, LOW FREQ EDDY CURRENT INSP CARRIED OUT AT BS 260 FR STR 18L TO 19L IN ACCORDANCE W/B727 NDT MAN 51-00-00 PART 6 FIG 5. SUSPECT MATERIAL LOS

Next page: https://openairdocs.org/model/boeing-727-30c/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 = '72730C'
ORDER BY difficulty_date DESC
```

This list as a web page: https://openairdocs.org/model/boeing-727-30c/reports

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